Modernizing a Shrike Commander
Transcription
Modernizing a Shrike Commander
Modernizing a Shrike Commander Dayton - Wright Brothers Airport 10570 Springboro Pike Miamisburg, Ohio 45342 Phone 888-881-5580 937-885-5580 Fax 937-885-5586 Web commander-aero.com email [email protected] Modernizing a Shrike Commander John Bosch and Gary Kromer Commander Aero had the unusual opportunity to purchase a Shrike that it had maintained for the past 15 years. It was as if we had owned the airplane because it was always in our hangar and we had the opportunity to give it plenty of TLC. When the owner transitioned to a turbo Commander he advertised for bids and Commander Aero was the successful bidder. Since the Shrike only had 2,700 hours TT and we knew that it was a solid airplane we had our hearts set on turning it into a modern airplane while retaining its classic attributes. From a project planning viewpoint we separated the project into five main categories. the airplane we had the test rerun. The test showed that we had a 36-month spar. After testing again with another company the results showed a 30-month spar. With this uncertainty we decided to replace the spar and eliminate the requirement for further testing. Fortunately we had experience replacing spars and had all the fixtures and skills to do the job properly. Major Tasks Aerodynamic Enhancements Avionics / Electrical Systems Special Features Final Dress-Up Russ Topp removing lower spar cap Jerry Cornett starting work on N741CA Major Tasks Three major tasks where identified that needed to be accomplished early in the refurbishment project. These were 1.) Spar replacement, 2.) Engine overhauls, and 3.) Gear inspection and overhaul. Spar Replacement A previous inspection resulted in the spar being identified as a 12-month test interval instead of the normal 36-months. After Commander Aero acquired Scott Shaw positioning new lower spar cap As a point of interest when the spar was removed from the airplane we examined it and found no evidence of corrosion. The testing procedures and equipment apparently are not able to differentiate between a good spar and one with defects or corrosion. Replacing the spar is a big job which is made even more difficult since it is necessary to remove the engines, engine mounts, landing gears, fuel cells, and the interior of the cabin. The Magnum Overhaul should be called a “ Re ma n ” wh e ny ou c on s i de rt h e de t a i lt h a tthe engine receives. All overhaul dimensions are c or r e c t e dt o“ f a c t or yn e w”t ol e r a n c e sa n df a rmor e new parts are installed than one would expect for an overhaul. The owner of Magnum Engines, Gene Svoboda is a perfectionist who keeps his shop as neat as the engines are at time of delivery. Russ Topp riveting the spar cap in place As part of the spar cap replacement task an inspection was made of the skins that were removed to determine if there was any evidence of corrosion. Where there was corrosion no matter how small the skins were replaced. We also replaced all fuel cells and installed new lift and turn fuel caps. Jerry Cornett performing SB222 on engine mounts New skin panels being installed Engine Overhaul CAI had the engines overhauled by Magnum Engines which is located within a few miles of Commander Aero. Their work is of the highest quality and it is convenient to transport engines from our hangar to their facility. Magnum engines are flow-matched at the cylinders and fuel system to assure that the combustion chambers receive an equal amount of fuel for optimum performance. Also the engines are dynamically balanced with the latest state-of-the-art computerized balancing equipment. While the engine is being rebuilt all engine components such as starters and oil pumps are sent to FAA approved specialty shops for overhaul. All new Lycoming cylinders were installed after they were polished and flow-matched. All new hoses were installed from the firewall forward and the baffling and brackets were repaired or replaced. In addition all wiring from the firewall forward was replaced. Engine and engine mount ready for installation Gene Svoboda, President of Magnum with N741CA Engine The engine mounts were inspected in accordance with SB 222, treated and painted to look like new. The inside of the cowling was also treated and painted. The final appearance of the installed engine made the airplane look even better than when it was brand new. Russ Topp mounting the engine Landing Gear Inspection Everyone who is familiar with twin Commanders appreciates the rugged construction of their landing gears. Little maintenance is required in order to The nose wheel gear actuator was rebuilt with a CAI seal kit and leak checked. The landing gear and wheel wells were painted making the gear assembly and wheel wells look like new. For final dress-up the original decals were installed making the gear look like the airplane was just being rolled out of the factory. New tires were mounted as well as new bungee Dick Kaercher cleaning gear components obtain reliable performance. But like any other mechanical component the gear and wheel wells are subject to wear and corrosion. We performed the 3000-hour landing gear inspection and replaced worn bushings and removed corrosion from the inside of the wheel wells and the landing gear components. cords. The landing gears were actuated multiple times to assure proper clearances between the gear mechanism and wheel wells. Gear components ready for paint and assembly Aerodynamic Enhancements There are two areas where aerodynamic improvements were made 1) installation of flap gap seals, and 2) installation of AeroDyne winglets. Flap Gap Seals provide early payback From strictly a performance and financial viewpoint the best modification that an owner can make to his piston Commander is to have flap seals installed. They are known to increase cruise speed by about 7 knots. This translates into a payback in approximately 250 hours flying time. Their advantage is that an area of drag is converted to an area of lift. Commander Aero produces its seals in accordance with its STC SA1566GL. We also have a PMA (Parts Manufacturing Authority) that provides us with approval to sell flap gap seal kits for other repair stations to install. We have many endorsements from owners attesting to the higher cruise speeds they have after installing flap seals. Bob Hoover had us install them on his Shrike and he became our best salesman. Bob was very pleased with the higher speeds he had with the gap seals and was pleased to give us permission to use his name as an endorsement. Winglets improve appearance The advantage of winglets on a 500S is primarily in the area of improved handling characteristics and better single engine performance. They also improve the appearance of the airplane. AeroDyne winglet with recognition light Flap Gap Seals installed on the underside of N741CA AeroDyne Winglets improve handling The winglets were installed with recognition lights and strobes. As most pilots know winglets reduce drag at the tip of the wings. The amount of drag is a function of the angle of attack. For piston aircraft flying at lower altitudes the angle of attack is relatively low making the reduction in drag less. For aircraft flying at high altitudes where the air is thinner the angle of attack is greater which makes the benefit of winglets greater. Aerodyne winglet installed on N741CA Most owners who retrofit their airplane with AeroDyne winglets purchase them with recognition lights. This is an important safety feature that provides an excellent outline of the aircraft. Avionics / Electrical Systems Avionic Upgrades Most of the excitement in general aviation today is the result of the latest advancements in navigation, weather and traffic/terrain awareness. Our customer, like so many other general aviation pilots, wanted to take advantage of these advancements. Flying is so much more fun i nt oda y ’ sc ompu t e ra g e . To begin the avionics upgrade project the entire panel was removed. All extraneous wiring and nonessential equipment was also removed. Not only was there a weight saving from this effort but the installation was much cleaner and future work easier to analyze because there is no confusion from unused wire bundles. All wiring and hoses were provided with service loops so the instrument panels could be tilted out at top for easy access behind the panels. Complete gutting of the panel Building a mock-up of the panel At the same time that used wires were removed all hoses in the cockpit and cabin area were replaced with new hoses. Any of the instruments that remained were sent to instrument repair shops for overhaul and certification. With this approach the complete panel could be considered new and there was confidence that the instruments were operating properly. While working in the cockpit area the pilot and co-pi l ot ’ sc on t r olwh e e l swe r ecleaned to look like new. The control columns were covered with the same leather used for lining in the cabin. Designing the panel The panel was designed with special software making it possible to quickly go through several iterations with the customer before arriving at the final layout. The autocad software was then sent by email to a local shop that cut out the aluminum panels with an automated laser machining center. Including the overhead panels there were a total of nine panels. After fitting checks the panels were painted and silk screened prior to installation. To optimize the panel during night flights Nulite wedge lighting components were installed for all the major instruments. This reduced clutter as well as making the instruments uniformly legible. Preparing internal wiring Checking for panel fit All new harnesses were made and there was no splicing of existing wiring that could cause a problem in the future. The objective was to have the same level of integrity in the entire electrical system as one would expect from a new airplane fresh from the production line. To help with future maintenance tasks communication jacks were installed aft of the baggage compartment so a technician in the avionics bay could talk to a technician in the cockpit. This facilitates making voltage adjustments or troubleshooting avionics systems. Tim Bench making harnesses Pilot panel and center console Co-pilot panel and center console To get the benefit of the latest avionic technologies the customer asked us to install dual Garmin GNS 480’ s , a Garmin TIS transponder, and a Castleberry flight director that we connected to the new S-Tec 60-2 autopilot with altitude pre-select and GPS steering. Switches were added to the overhead panel for strobes and recognition lights located within the AeroDyne winglets. The list of avionics is impressive: New Garmin AT MX20 with Traffic & Chart View New Garmin AT Dual GNS 480 WAAS GPS/NAV/COM Systems New Garmin GTX 330 TIS Transponder New Garmin AT SL70R Remote Transponder New Garmin GMA340 Audio Panel with Marker Beacon and 6-place Intercom New S-Tec 60-2 Autopilot w/ GPSS steering, ST-360 Altitude Pre-Select & Flight Dir. New EII Digital/LED Engine Gauges New L3 WX 500 Stormscope New WSI InFlight Weather New SHADIN ADC 200 New SHADIN DIGIFLO fuel flow system New Custom Instrument Panels with Silk Screening New Nulite Wedge Lighting Plus RDR 2000 Stabilized Color Radar with Vertical Profile (Displayed on MX20) Collins HSI Insight Gemini Engine Monitoring System Davtron Clock Smaller light bulbs were used for the annunciator function to save space and also to make the panel look modern. Flight Safety Priority Safety of flight was a priority in the selection of systems and the design of the panel. With advancements in avionic equipment every effort was made to overcome and avoid problems with weather, traffic, terrain and the possibilities of instrument or electrical failures. Center console With this in mind the following selections were made: Du a lGNS480’ sf orr e du n da nc y Traffic Avoidance - Garmin TIS system Weather Bendix RDR 2000 Radar L3 WX 500 Stormscope WSI In-Flight Weather Garmin AT MX20 moving map & MFD with terrain displayed Fuel Management Dual transponders for redundancy Emergency avionics bus Whelen 3-light strobe system –Comet flash Annunciator warning system All pilots are aware that weather is the major factor in flight safety and knowing the weather ahead is critical. To get this information the owner selected radar for detecting precipitation from a horizontal view, a Stormscope to detect electrical discharges from opposing air currents, and satellite weather to observe weather patterns from a vertical view. These displays along with visual observations will give the very best information about the weather. Special Features The owner of N741CA wanted five special features for his airplane. 1.) TKS De-Icing system, 2.) TurboCharging, 3.) Built-In Oxygen System, 4.) Extended baggage compartment, and 5.) Engine, Battery and Cabin Heaters. Only one choice exists for the pilot while operating the ice protection system: anti-ice or de-ice mode. In the anti-ice mode, a protective film of glycol prevents the formation of ice. In the de-ice mode, the glycol chemically breaks the ice bond. A significant feature of both modes is the elimination of run back ice. TKS De-Icing system The owner had previously owned a Bonanza with the TKS weeping wing de-icing system. He really liked it and wanted the same system for his Shrike. TKS“we e pi ngwi ng”i ns t al l e d Russ Topp installing the TKS leading edges Porous, laser drilled titanium panels are installed on the leading edges of the wings, and horizontal and vertical stabilizers. A slinger ring is installed on the propeller and a spray bar is positioned on the windshield for protection. A glycol based fluid is exuded through the panels and flows over these surfaces keeping the aircraft virtually ice free. The weight added to an aircraft as a result of the TKS ice protection installation is minimal. The TKS system weights approximately 40 lb without fluid (lighter than a rubber boot system, if one was available) and approximately 100 lbs with a full tank of fluid. The attractive TKS system requires a minimum of upkeep. As the system is used, it flushes out any accumulation of debris on the panels. Glycol, the main ingredient of the ice protection fluid, has cleaning properties and will not harm the paint finish on the aircraft. Filler Cap for De-Icing Fluid The glycol based fluid is metered from a tank by a small electrically driven pump through a microfilter to proportioning units. The proportioning units contain calibrated capillary tubes which apportion fluid to the individual panels and the propeller slinger ring. The windshield is protected with an on-demand pump and spray bar. A significant advantage for the pilot is the simple operation of the system. Just turn the system ON when icing is encountered and OFF when leaving icing conditions. TKS leading edges on the tail There is absolutely no loss in aircraft performance as a result of installing the TKS system, yet significant anti-ice and de-ice capabilities are added. Up to 3.0 hours of continuous anti-ice protection is possible with a full tank of ice protection fluid. The placard “ Th i sa i r c r a f ti sa ppr ov e df orf l i gh t i n t okn owni c i ng . ”says it all. Turbo-Charging Because the owner would be flying over the Rocky Mountains he wanted the engines to be turbocharged. After evaluating what was available the Merlyn Products turbo system was selected. Merlyn Products Turbo System Seeing a need to replace the old turbo systems of the past, Merlyn Products has provided the Twin Commander 500B, S, and U owners with a new alternative for gaining performance from their current E1A5 or E1B5 engines. The turbo-normalized system uses a single high efficiency Garrett turbo per side providing a full 290HP at 18,000 feet. Airspeed is 190KTAS at 12,000 feet and 70% power. Single engine service ceiling is 14,000 feet and takeoff and climb performance is improved. Fuel flows are unchanged and there are no scavenge pumps and no operating limitations. The kit includes new exhaust, hoses, and induction tubes. Incorporation of the STC (SA01142SE) is available with a 250lb gross weight increase. Built-In Oxygen System The built-in oxygen system provides convenience and looks first rate in the all leather interior. The system is extremely easy to use. The regulator is located where it can be reached by the crew or passengers in the forward part of the cabin. After the supply cylinder is opened the masks may be connected to the outlet ports. The large knob on the regulator is a dj u s t e df ora l t i t u de .I t ’ si mpor t a n tt o remember not to smoke while oxygen is in use and to turn off the flow of oxygen at the regulator before disconnecting the masks from the outlet ports. The supply cylinder is located in the aft fuselage adjacent to the avionics racks. Complete new exhaust is above the engine Merlyn has taken advantage of advancements in turbo charging systems by producing a kit that is efficient, lightweight, and simple. And does it ever ma k et h e powe r ;30” MAP a t18, 0 00 f eet. No modifications are needed to the airframe. Oxygen regulator and outlet shown above co-pi l ot ’ ss e at The crew and passenger masks are stowed conveniently in the cabin for use whenever flying at higher altitudes. Oxygen outlets are next to each seat for six occupants. Turbo is mounted aft of the engine Extended Baggage Compartment The owner is a sportsman who has many interests including skiing. To carry his skis he wanted an extended baggage compartment. This is a feature that we have provided for other customers by enclosing space from the current baggage compartment back to the battery bay. This increases the baggage compartment capacity from 27.1 ft.3. to 38.2 ft.3 for a 41% increase. Perhaps even more important it provides a space for stowing items like skis or rifles that are up to 6 feet in length. The baggage compartment and the extended portion are lined with gray leather and the floor is carpeted. Engine, Battery and Cabin Heaters With the owner living in Minnesota there is need to have heaters for winter flying. Most importantly oil heaters were installed on the engine sump and the cylinders plus the batteries are wrapped with a heating pad. For the comfort of the crew and passengers electric heated mats are placed on the carpeted floor to warm the cabin. An external power jack is conveniently located next to the battery compartment. External power connector and battery compartment Interior of baggage compartment Just inside the baggage compartment in the upper right hand corner are lights that show the Tanis heaters are on. Separate lights are for LH engine, RH engine, battery, and cabin. Below the lights is a switch to turn off the cabin heat. This is important if a remote airport has limited electric current the priority is to heat the engines and battery. Final Dress-Up Extended portion of baggage compartment To make it easier to place long items in the extended portion of the baggage compartment the baggage door hinges were changed from being on the forward side of the door to the upper side of the door. FAA approval was granted to make the alteration. An air cylinder was used to lift the door after it is unlatched and a light on the door illuminates the area in front of the door to make loading and unloading luggage at night an easier task. The lights internal to the baggage compartment and the one on the door turn off when the door is closed and latched. With the objective of making N741CA the best Shrike in the world there was no item too small for us not to make it the best possible. With this in mind everything was done to make each function and part be exceptional. This was important not only from an appearance point of view but also from a convenience and usefulness consideration. Fresh JetGlo paint on N741CA Exterior Paint The airplane was painted by Cimarron of El Reno, OK. The paint scheme was selected by the owner that features a double gold strip and cream background. NASA Foam seat cushions Arm rest in the middle of the rear bench seat Cabin Interior While attending a NBAA convention considerable time was spent selecting leather goods for the cabin interior. A high-quality leather material was chosen that is intended for the best executive jets. There were two thicknesses of leather selected. The thicker material is for the seats and the thinner material is for the side and top liners. For carpeting a fire retardant fabric was chosen of a dark gray that complements the lighter gray leather seats. Before the final installation of the interior we applied a super sound proofing material and membrane to keep the cabin as quiet as possible. Seat Cushions and Seat Belts For the ultimate in comfort NASA foam was used for the pilot and copilot seat cushions. To help keep the cockpit organized during flight storage pockets were i n s t a l l e dont h epi l ot ’ sdoora n donbot hthe pilot and copilot seats. Shoulder belts for the pilot and copilot are included along with lap belts. In addition to belts for the crew there are 5 lap belts for passengers, 2 for the rear facing seats and 3 for the rear bench seat. For the comfort and convenience of passengers a large arm rest is provided between the seats on the rear bench. As with most arm rests it can be lifted up to make space available for a third person to sit in the middle of the rear bench. Entertainment Jacks Entertainment Jacks Each seat has a panel for entertainment and communication jacks. Passengers have the ability to listen to the crew talking to ground control or to talk to the pilot. They also have the ability to listen to music from the entertainment jack by bringing along a CD player or other recorded music player. Storage pocket i npi l ot ’ sd oor Personalized Gust Lock Commander Aero is an advocate of always using a gust lock when a Commander is on the ramp. With this in mind CAI designed its own gust lock to be easy to install and remove. This is done with one hand while standing on the ramp. Passenger amenities Convenience Features Opposite each seat there are air outlets, individual lighting and an adapter for oxygen masks. The creature comforts and cabin interior were planned to be similar in luxury to a Citation. N741CA Ready for Take-off Commander Aero has much pride in N741CA and feels grateful for the opportunity to have worked with Dr. John Trusheim who is the owner. His desires for additional features helped make N741CA the exceptional airplane that it is. Together we have set a new standard for modernizing twin Commanders. Stow-Away table If passengers want to write a note, use a laptop computer, have a snack or play cards there is a convenient stow-away table available. About the authors John Bosch is president and Gary Kromer is service manager at Commander Aero. For more information on these upgrades or other information contact Gary or John at 888.881.5580. Rudder Gust Lock