Cirrus sr maintanence manual

Water wash - Any Source Cleaning of surface. Rubber Roller - Any Source Application of surface pressure. Refer to 4 Remove protective backing from decal using care not to contaminate adhesive surface.

Avoid stretching decal as poor adhesion will result. Ensure all edges are firmly adhered. Exterior Placard Removal. Excessive heat may result in loss of structural integrity. The remaining placards are printed on cast vinyl.

Clean, white, lint free cloth - Any Source Solvent Wipe. Hot-air blower - Any Source Removal of panel.

Putty knife - Any Source Removal of panel and residual adhe- sive. Refer to c Apply heat with hot-air blower until adhesive loosens from panel surface. Refer to 2 Installation - Polycarbonate Graphic Overlay a Acquire necessary tools, equipment, and supplies. Rubber Roller - Any Source Application of sur- face pressure. Refer to c Remove protective backing from one half of overlay using care not to contaminate adhe- sive surface.

Refer to d Remove protective backing from decal using care not to contaminate adhesive surface. GENERAL The information in this chapter pertains to general servicing procedures and maintenance practices used when servicing the airplane.

This chapter contains illustrations, descriptions and servicing procedures nec- essary to locate system or component service points and to replenish operating fluids or service the air- plane as required. See Figure The replenishment charts provide tank and reservoir capacities.

Where applicable, capacities are listed in U. Gallons, Imperial Gallons, and Liters. For additional detailed information concerning unit servicing of the various airplane systems and components, refer to the applicable chapters. For electrical wiring dia- grams, refer to the Wiring Diagram Manual.

The specified intervals in Chapter 5, are considered adequate to meet average requirements under normal operating conditions. It is advisable, however, to shorten service and maintenance intervals when operat- ing under abnormal environmental conditions, such as high humidity and moisture, salt water environ- ments, dusty atmospheric conditions, extreme temperature ranges, unimproved airport facilities, or other unusual operating requirements. In salt water areas special care should be taken to keep the engine, accessories and airframe clean to help prevent oxidation.

CAUTION: The operation of the airplane can be seriously impaired if unapproved or contaminated fuel, oil, fluids, lubricants or materials are used. Adherence to instructions, cautions, and warn- ings can avoid injury to personnel and damage to the airplane or associated equipment. Mix- ing of various brands, types and weights of materials should be avoided.

Specified lubricants will meet requirements for extreme hot or cold temperature operations. Use of substitutes or other lubricants may cause a malfunction when operating in extreme tempera- ture conditions, or may cause excessive wear due to improper lubrication. As called out in the illustration, stepping or walking on most of the airplane outer surfaces is prohibited. Fuel System 1 Safety Precautions.

Ground exhaust pipe outlet and fuel service equipment prior to every fuel- ing and defueling procedure. Check wing fuel tank vents for obstruction before refueling.

Do not fill tanks within feet Do not smoke or allow smoking or open flame within feet Do not operate electronic equipment or electrical switches during the fuel- ing or defueling procedure. Frequently check fuel for ice formation during cold weather operation. Sample fuel after each refueling and before the first flight of the day for any moisture or contaminates. Wait at least five minutes for any moisture and sediment to settle before flushing fuel drain valves.

The use of lower octane rated fuel can result in destruction of an engine the first time high power is applied. If the airplane is inadvertently serviced with the wrong grade of fuel, the fuel system must be completely drained, properly serviced, and the proper engine inspection completed.

Engine inspection should be performed as indicated in the Teledyne Conti- nental Motors Overhaul Manual. Left wing Total Rubber protective cover - Any Source Protect finish of airplane. Keep fuel tanks full at all times to minimize condensation and mois- ture accumulation in tanks. In extreme humid areas the fuel should be checked frequently and drained of condensation to prevent potential prob- lems. Note: If fuel is going to be added to only one fuel tank, the tank being serviced should be filled to the same level as the other fuel tank.

If the fuel level is filled to the fuel level tab inside the fuel tank , there will be approximately 23 usable gallons A filler cap with an integral dipstick is provided for determining the amount of oil in the crankcase. If engine oil must be added to the factory installed oil, add corrosion preventive mineral oil conforming to MIL-L Mixing oils of various specifications should be avoided.

After 25 hours of operation and after oil consumption has stabilized, use only avi- ation lubricating oils which are ashless dispersant. Straight mineral oil conforming to MIL-C with a corrosion preventive com- pound added, can cause coking with extended use; therefore Cirrus Design does not recommend its use for break-in or post break-in.

Note: Oil level should always be checked with the airplane sitting on a level surface, with the engine off.

Verify engine oil level. Minimum oil quantity is 6 quarts 5. Hydraulic Brake System The main wheels have hydraulically operated, single-cylinder dual piston type disc brakes, individually activated by floor mounted toe pedals at both pilot stations.

A parking brake mechanism holds induced hydraulic pressure on the disc brake for parking. The system is replenished by filling the hydraulic res- ervoir, located in the engine compartment on the upper right corner of the firewall. Replenish the sys- tem with MIL-H hydraulic fluid only.

Fluid in the wheel cylinders may be under high pressure due to expansion. Therefore, be sure parking brake is released and wheel chocks are in place, prior to beginning hydraulic system servicing. If the brake pedal feels spongy, the complete brake system must be bled. If the system is low, the reason for fluid loss, must be deter- mined before continued operation of the airplane. Any spilled brake fluid must be removed immediately as it will damage any painted surface upon contact.

Remove any dirt on the brake fluid reservoir filler cap before opening. Refer to b Remove any dirt from the hydraulic brake fluid reservoir before opening the filler cap.

Refer to D. Tires The nose tire uses a 5. The main landing gear uses 15 x 6. Always keep the tires inflated to their rated pressure to assure maximum service and to reduce damage when landing on stones with sharp edges.

When adjusting tire pressure, inspect the tires for any signs of abnormal wear, cuts, or bruises. Compressed air supply - Any Source Adding air pressure to tires.

Accurate air pressure gage - Any Source Checking tire pressure. Wheel chocks - Any Source Securing airplane. Always check air pressure using an accurate gage. Note: Always consider load factor and ambient temperature when checking air pressure. Air pressure will increase when the tire is subjected to a load and when the temperature increases. Always service tires in a warm environment, this will keep the valve stem from freezing and eliminate the possibility of leaks through the valve core.

After inspecting or adjusting tire pressure, always inspect the valve core for leaks before reinstalling the valve cap. Always install a valve cap to prevent contaminates from entering the valve core. Place wheel chocks in position. If the tire is currently over inflated, push in on the valve core and release some air until the correct pressure is obtained.

Battery System Two batteries are used on this airplane for energy storage. Battery 1 is located in the engine compart- ment on the forward right side of the firewall and is the only battery which the electrolyte level can be adjusted. Access to the battery can be accomplished by removing the upper engine cowling.

With the exception of the electrolyte level check on battery 1, there are no on-airplane replenishing require- ments for the batteries.

Battery 2 is located just aft of bulkhead and is considered a maintenance free battery. Proper battery charging procedures for both types of batteries, and the replenishing of electrolyte for battery 1, along with other pertinent information can be found in Chapter Metal objects may fuse to electrical connections and cause severe burns. Acid should never be added unless the electrolyte has been lost by spillage, because the acid does not evaporate.

When it is necessary to add acid, the battery should be fully charged, on charge and gassing freely. Specific gravity then may be adjusted by adding acid or distilled water, or drawing off electrolyte. The electro- lyte should barely touch or be slightly short of the eyelet level indicator when the battery is warm and in a good state of charge.

As an example, this condition would exist just after a bench charge or when the aircraft has just returned from a flight of ninety minutes or more. Refer to e Reinstall battery into airplane. Servicing the fuel system, lubrication system, tires, brakes, and battery are covered. Cleaning of interior and exterior surfaces are also covered. Fuel System 1 Drain Valves Five fuel drains are provided throughout the fuel system to drain fuel, water or sediment from the fuel system.

A fuel-drain valve is located on the underside of each wing, directly beneath each fuel tank to provide drainage of moisture and sediment. The two integral collector tanks and the gascolator also have a flush drain valve. Use the fuel sampler cup to remove fuel and any con- taminates from the collector tanks and gascolator.

If the possibility that air has entered the system does exist, start and operate the engine on the ground until all air is removed from the system. Operate the engine for several minutes on each tank until proper engine operation is assured. Ground the exhaust pipe outlet, fuel service unit, and servicing nozzle, prior to all fueling and de-fueling operations.

Operation of any electric switch other than the master battery switch and the electric fuel pump switch is prohibited during the de-fueling operation. Operation of any electric switch during the fueling operation is prohibited. Smoking or open flames within feet Do not operate radios, electric system or electronic equipment during the fueling or de-fueling operations.

Do not drain fuel tanks within feet A fire extinguisher must be available. Fuel drain container - Any Source Drain old fuel in.

Hand operated pump - Any Source Siphon fuel. Ground airplane to a suitable earth ground. Remove filler cap. Install filler cap. If the possibility that air has entered the system exists, start and operate the engine on the ground until all air is removed from the system. Refer to i Inspect the complete fuel system for any signs of leaks and service as required. Fuel drain container - Any Source Drain old fuel into. Fuel drain hose exten- - Any Source Drain fuel sion. Allow the fuel pump to operate until the fuel tank is empty, then set switch off immediately.

Repeat steps 7 and 8 until the remaining fuel tank is drained. Refer to o Inspect the complete fuel system for any signs of leaks and service as required. If the possibility that air has entered the system does exist, ground run the engine on the until all air is removed from the system. Refer to j Inspect the complete fuel system for any signs of leaks and service as required.

Hydraulic Brake System The brake reservoir is located on the right side of the firewall in the engine compartment. The brake system is filled with MIL-H petroleum base hydraulic brake fluid red. The fluid level should be checked periodically and at every inspection and replenished when necessary. If the entire system must be filled, fill with fluid under pressure from the brake end of the system.

This will eliminate air in the system. If the system is low, the reason for loss of fluid must be determined before continued oper- ation of the aircraft.

For additional brake information refer to Chapter Refer to Fluid in the wheel cylinders may be under high pressure due to expansion. If the system is low, the reason for. After oil consumption stabilizes the mineral oil should be drained and an approved engine oil used. In a laboratory study, mice developed skin cancer when their skin was exposed to used engine oil twice a week, without being washed off. Substances found to cause cancer in laboratory animals may also cause cancer in humans.

Never fly the airplane with less than 6 quarts of oil 5. Oil consumption tends to be higher during break-in periods on new engines. Under no circumstances should automotive oil be used, for such oils could cause engine damage. If the oil sys- tem becomes contaminated, the complete oil system must be flushed and the oil cooler replaced. Do not mix additive oil and straight mineral oil. The engine must be thoroughly warmed, prior to draining the oil from the engine.

Always change the filter when changing oil. This is especially important when changing from straight mineral oil to compounded or addi- tive oil. After changing from straight mineral oil to compounded or additive oil, inspect the oil filter for evidence of sludge, if sludge is evident, replace the oil and filter more fre- quently.

Resume normal oil drain intervals after sludge conditions improve. Note: During periods of prolonged operation in dusty areas or in cold climates, or when flights have been of short duration with prolonged idling time, change oil and filter every 25 hours. The engine should always be brought to operating temperature prior to draining the oil to assure complete draining of the oil.

The engine oil filter and drain plug is secured with safety wire. Check every used oil filter for metal particles and sludge.

Oil drain pan - Any Source Retrieve used oil. Safety wire,. Tension safety wire. Flexible oil funnel - Any Source Replace engine oil.

Refer to c Place a suitable drain pan under the drain plug. Note: A flexible oil funnel can be used to aid the draining process. Allow the oil to completely drain out. Tighten the filter to ft.

Refer to g Safety wire oil filter. Tighten the oil drain plug to 17 ft. Refer to j Fill the engine oil sump with an approved oil. Allow the engine to idle for a few min- utes and shutdown the engine in accordance with POH procedures. Correct any leaks found immediately. Verify engine oil level, add oil as needed. Tighten the knurled head screw until the cutter blade meets the filter metal can surface.

Continue tightening the knurled head screw and rotating the cutter until the filter mounting plate is free from the canister. Cut the filter material from the end caps. Tires and Wheels Replace all worn tires with the correct ply, type, and size ratings. Tire servicing is covered in chapter Refer to For tire and wheel removal, installation, and inspection procedures refer to Chapter Recapped tires have a tendency to swell as a result of the increased temperature generated during take- off.

Note: If the airplane tires should ever freeze to the ground surface, use hot air or water to free the tires before attempting to move the airplane. Battery Visual inspection of battery 1 in the aircraft should be done every month or 25 flight hours until experi- ence indicates a longer inspection interval.

Check the battery, container, cover and connections for dis- tortion or damage. Proper battery charging procedures and the replenishing of electrolyte, along with other pertinent information for battery 1 can be found in Chapter Refer to F.

Lubrication Lubrication and cleanliness should always be considered to be of utmost importance. To prevent rapid and unnecessary deterioration of metal components which are exposed to the elements of nature, the following should always be clean and lubricated. Only use lubricants recommended by the manufac- turer. Keep threads free of grease to avoid degrading lock nut performance and torque readings. Only use lubricants recommended by the manufacturer.

Seat tracks hours Paraffin Wax - Any source. Trim cartridge hours Dry Lube - Any source. Cleaning To maintain the flying characteristics of the airplane, the external surfaces of the airplane and propeller must remain clean, especially the leading edges of the wings. To aid in protecting the finish, insect res- idue should be immediately washed off after every flight.

For best cleaning results on cured paint, paint that has been in a warm climate for at least 90 days after being applied and prior to being washed with hot soapy water use a generous amount of fresh warm water.

If necessary, a mild non- abrasive aircraft cleaning agent may be used. Apply a heavy coating of silicone-free wax to the leading edges of the nose section, wings and empennage. If any points of lubrication are washed away, they must be lubricated immediately after washing. Approximately once a year, the exterior painted sur- face of the airplane should be waxed and buffed using a good quality silicone free automotive wax.

CAUTION: Because wax seals paint from the outside air, a new paint job should not be waxed for a period of 90 days, in order to allow the paint to fully cure. Wash uncured painted sur- faces with only cold or lukewarm water and a mild non-detergent soap. Any rubbing of the painted surface should be done gently and held to a minimum to avoid cracking the paint film. Always test wash an inconspicuous area first, to determine the compatibility of the cleaning agent being used.

Do not use household detergents to wash the exterior of the airplane, or damage to the finish may occur. Do not wax, use hot water, or apply soap to uncured paint, paint which is less than 90 days old or damage to the finish may occur. Some household spray cleaners may damage aluminum and other materials, always refer to the manufactures instructions for proper usage for the product being used. When washing the airplane with mild soap and water, use special care to avoid washing away grease from any lubricated area.

After washing with solvent in the landing gear area, lubricate all lubrication points. Premature wear of lubricated surfaces may result if the above precautions are not taken. When fuel, hydraulic fluid, or other fluids contain- ing dye are spilled on any painted surface they must be removed immediately to prevent staining. Automotive paste wax - Any Source Waxing exterior of air- silicone free plane and acrylic win- dows. Cotton cloth clean - Any Source General cleaning white, lint free.

Never allow any of the aforementioned orifices to remain obstructed or restricted. If any obstructions or restrictions are found they must be corrected before the airplane is allowed back into ser- vice.

Never rub dry acrylic. Dull or scratched window coverings may be polished using a special acrylic polishing paste. Only clean acrylic windows with an antistatic acrylic cleaner.

Remove grease or oil with a soft cloth saturated with kerosene. Polishing inner window Jeannette, PA surface. Cotton cloth clean white, - Any Source General cleaning proce- lint free dures.

Kerosene - Any Source Grease and oil removal. CAUTION: Never use de-icing fluid, household window cleaning sprays, lacquer thin- ner, gasoline, acetone, carbon tetrachloride, benzene, or fire extinguisher fluid to clean windows or windshields. The use of such chemicals will soften or craze an acrylic surface. Never use rain repellent on acrylic surfaces. Always cover the windshield and windows when applying any chemicals near the vicinity that may damage them.

Never use sun shades or allow sun visors to remain in the lowered position when the airplane is parked in direct sunlight or crazing and the formation of bubbles may occur. Note: Prior to cleaning windows, place the airplane in a shaded area to allow the windows to cool down.

When polishing an acrylic surface, use a polish meeting Federal Specification P-P While vacuuming, use a fine bristle nylon brush to help loosen par- ticles. Carpet may be cleaned like household carpet made with the same composition and simi- lar weave. The headliner is made from polyester. The headliner can be cleaned using the same methods for cleaning any object made out of polyester.

For smudges from dirty hands or tools, powdered laundry soap can work well. The instrument panel, control knobs, and plastic trim need only to be wiped clean with a soft damp cloth. Do not use alcohol or other strong solvents on interior plastics. Never allow alcohol to enter microphone or electrical connections. The interior fur- nishings can be easily damaged if cleaned with Methyl Ethel Ketone MEK , naph- tha, mufti standard solvent, gasoline, lacquer thinner or other types of thinner.

Never saturate any fabric with solution which could damage the backing or pad- ding materials. When cleaning carpet, keep the foam as dry as possible and rub the carpet in circular motions. Never allow carpets to remain damp; always dry them thoroughly. Always follow the manufactures instructions on proper usage of their products. Compressed air is not recommended for cleaning the headliner.

Saddle soap - Any Source Clean leather surfaces. Mild dishwasher soap - Any Source Clean leather surfaces Abrasive free. Cotton cloth clean white, - Any Source General cleaning procedures lint free. Whiskbroom - Any Source General cleaning procedures.

Vacuum cleaner - Any Source General cleaning procedures. A dirty engine com- partment will also hamper the inspection process. Always inspect engine for leaks, loose hardware, and worn hardware prior to cleaning. Always cover all win- dows, magneto vents, engine electrical components and connections when wash- ing any portion of the engine compartment. Remove the air filter and cover the air induction inlet prior to washing the engine compartment.

Never use any flamma- ble or corrosive cleaning solvents. Never allow the airplane to sit in freezing tem- peratures until the airplane has thoroughly dried. Cotton cloth clean white, - Any Source General cleaning lint free. Refer to c Inspect engine for leaks, loose hardware, and worn hardware.

Service as required. Refer to e Cover the alternator, starter, vacuum pump, and air induction intakes. Refer to k Remove the catch pan from under the engine. Leather Interior Leather is the most durable and easily maintained upholstery material available.

Like most other important investments, leather requires routine maintenance. For routine maintenance, occasional wiping with a soft, white, damp cloth is all the care your leather will need. The approved leather care products are available from Cirrus Design. It will safely and effectively remove dirt, grime, and soil. It will remove some ink marks and grease stains; however, for stubborn ink marks and stains, use the ink remover available from Cirrus Design.

The approved leather conditioner cleans, conditions, and restores. Especially formulated to remove surface dirt and enhance the luster of naturally tanned leather, the unique wax-free for-. It also provides emollients, color restoration, water retardation, and ultraviolet ray protection, which decreases color fading. If applied regularly, the conditioner will enhance the natural luster of fine leather, while increasing the longevity of the product. The approved leather conditioner is safe for use on all colors.

Leather cleaner and leather conditioner were developed for use on protected or semi-aniline leather. Never use leather cleaner or leather conditioner on suede napped or pure aniline leathers.

They can also cause leather to age prematurely by causing weakness, cracking, and discoloration. Not all cleaning products suggested for leather will protect and preserve the life of your upholstery. Test in an inconspicuous area to ensure colorfastness. Never apply product directly to upholstery. Some stains can cause permanent discoloration even after cleaning. Never use the leather care kit in conjunction with cleaning products not approved by Cirrus Design. House cleaning liquid Whisk Any Source Remove fresh baby oil, ketchup, grape juice, coffee or tea stains.

Spray cleaning solution Fantastik or Any Source Remove fresh crayon or grease stains Ammonia - Any Source Remove fresh lip- stick or yellow mus- tard stains. Note: Always clean stains immediately as some inks and stains set faster than others. Always follow the directions from the manufacture of the cleaning agent being used.

Leather care kit Cirrus Design General leather care. Leather cleaner Cirrus Design Cleaning leather. Leather conditioner Cirrus Design Conditioning leather. Spot and stain remover Cirrus Design Removing spots. Vinyl finish vinyl cleaner Cirrus Design Cleaning vinyl. Coffee 1 Tea 1. Clean with a mixture of Whisk House Cleaner Liquid and water. Rinse with clean water, and dry. Snow and Ice Removal: Snow and ice must never be allowed to remain on the airplane.

If snow or ice have accumulated, it is recommended to remove it by placing the airplane in a heated hanger. This will prevent melted snow and ice from refreezing on the surface, or in any gaps. Never use de-icing fluids to remove snow deposits from the airplane. Heated de-icing fluids can damage composite structures from the extreme temperature change.

Some de-icing fluids may damage acrylic windows. Most anti-ice additives contain ethylene glycol monomethyl ether EGME. Anti- icing additives containing ethylene glycol monomethyl ether can be extremely harmful if inhaled, swallowed, absorbed through the skin, or if eye contact is allowed. Vapors from EGME are dangerous to health when breathed or allowed to absorb into the skin.

If EGME contact is experienced, the following emergency and first aid procedures should be followed. If EGME is inhaled, remove the person to fresh air. If the person is not breathing, give mouth-to-mouth respiration.

However, if breathing is difficult, administer oxygen. Always call a physician. If EGME is swallowed, drink large quantities of water, then induce vomiting by placing a finger far back into the throat. Contact a physician immediately. If vomit- ing cannot be induced, or if the victim is unconscious or in convulsions, take this person to a hospital immediately. Do not induce vomiting or give anything by mouth to an unconscious person. If EGME has contacted the eyes, flush with plenty of water for at least 15 minutes.

If EGME has contacted the skin, remove all contaminated clothing and wash affected areas with soap and water; then call a physician. Wash all contaminated clothing before re-use. Instructions necessary for proper usage and identification of special tools, thread lock and fastening hard- ware are also provided. Sealant is used to prevent the spread of fire or flames from the engine com- partment to the airplane, prevent air leakage, prevent fastener corrosion, prevent water or dust intrusion, and to prevent fluid leakage.

The following sealants are recommended by Cirrus Design Corporation. Approved Sealants The sealants shown in the referenced figure, when applied properly, have been approved by Cirrus Design for use in specified applications. These sealants are available from a variety of manufacturers and packaged in a variety of fashions - in bulk, in kits, and in premixed form. Shelf Life Shelf life refers to the period of time usually from the date of manufacture in which the sealant is usable.

Shelf life is dependent on proper storage temperature and environmental factors, such as humidity and exposure to sunlight. Storage Criteria All sealants must be stored under controlled temperature conditions to achieve maximum shelf life. Note: Containers must be tightly closed prior to placing them in the proper storage environ- ment. Sealants must be stored as recommended by the manufacturer. Mixed sealants subjected to refrigerated storage may exhibit altered application life.

Use of a quick-freeze technique is rec- ommended to minimize the amount of application life that would be lost in a slower cooling pro- cedure. To quick-freeze mixed sealant, immerse the filled cartridges in a slurry of dry ice and alcohol for 10 minutes. The time con- sumed by freezing and thawing operations reduce application life by approximately 30 minutes. Further reduction in application life may result from duration and temperature during storage.

It is recommended that all aspects of mixing, freezing, and thawing be considered before mixing and freezing material with less than one hour application life. Supplier Application. Dapco Sealant Anaheim, CA. Thread Sealant 50 ml tube Loctite To obtain a leak-free seal on non-fuel system metallic pipe threads. Work life is specified by adding the desired work life in the product dash number after the Class designation, e.

Results can vary due to temperature, humidity, and mix proportions. Testable cure time based upon a Rex Durometer reading of at least 30A to 35 A. All sealants must extrude freely before application to any surface. High humidity during the mixing process will shorten application time.

Tack-Free Time Tack-free time is the time that a sealant requires to cure sufficiently to not stick to standard polyethyl- ene film when the film is pressed into the sealant. Cure Time The time require to sufficiently cure applied sealant depends upon the ambient temperature and rela- tive humidity.

Low humidity will extend the cure time. A high state of cure is developed after 14 days at this temperature and humility. This section describes those components used for computing data from a number of different sources. This includes the GIA 63W integrated avionics. The main processor interfaces with all of the Per-.

The integrated avion-. For an. Refer to. Download Toyota Vitz Manual. Install countersunk screws securing pick-up collar support to pick-up collar. Using large strap wrench at top of rocket motor case, slightly rotate rocket motor case clockwise while observing exposed tip of Ortman key. As tip of key retracts into rocket motor case, continue to rotate rocket motor case until key is completely retracted. Rocket Motor Case 2.

Upper Propellant Grain 3. Lower Pro … Control dust migration. Ensure bottom of line cutter is not dire … Cable Tie 2. Corrugated Loom 3. Forward Cable Tie 4. Middle Cable Tie 5. Aluminum Tape 6. Wipe away over-squeeze. Feather adhesive to fuselage contour.

Use utmost care when working around embedded forward harness straps and lightning protection mesh with sharp tools. Measure Measure 8. Mix material thoroughly.

Do not pinch harness between spacer and three-point shackle. Install nuts on inboard side of shack- les. Torque nuts to 95 - in-lb Bolt 2.