Bellanca 17-30A Maintenance Manual

chemically stripped, etched, and allydined on both SIDES/ALL rear (the internal surfaces were then zinc chrome, primed) the outer zinc surfaces are chrome, primed and prepared for recycling. The total remaining exterior of the aircraft was stripped of its original final finish, including all the bottom without damaging the process, to the original silver ultraviolet protective coating. Any discrepancies have been corrected at the plant approved process and materials, including to step up the process, proper plumage from all areas needed. The aircraft was chemically cleaned after training and primed as needed before the final finish. All exterior parts previously taken were painted separately off the aircraft. The aircraft was carefully disguised to prevent it from being washed in undesirable areas. The glider received three common layers of Imron (paint numbers and colors to be listed) on the original four-color factory paint scheme and measurement using Bellanca factory original drawings. This includes all properly placed new decals including the bottom and chassis decals (after the chassis repair) (a separate entrance later). All previously removed and improved parts have been reinstalled using all new equipment, stainless steel screws, where applicable. New upper and lower locks, equipment, etc. were used. All new Plexiglas, landing lens and navigation light dozens have been installed with the factory new parts. A new rubberized ribbon of the front edges on the rear horizontal stabilizers and persistent brackets has been installed. New lower-side communication antennas have been installed to reduce resistance and improve the appearance. A re-chromated pit tube and new equipment have been installed. The refined wing is walking to the original appearance. Numerous other different details are completed. The propeller is being rebuilt and perfected into a new configuration, decals, etc. The base color is white #55769U Vol. LE 4.9 Vol AP 4.9. The first color finish burned orange #7455 modified to the next to lighten the color: #555U white at 98.0 #53U Jet Black 159.0. #557U. Fast Red 815.5. #547U Orange 2496.5. The second finish is beige #78390. The stripe of the pin is orange #1021. All colors of Dupont Imron. Door cabins and luggage doorways were perfected in a base coat of white #55769U. Inside both Fuel tanks doors have been prepared and refined to the original color. New fuel caps have been installed and inside decals as needed. The Auxillary fuel tank door is prepared and refinished inside including a lid and the necessary decals. New front screens of edge vents have been installed Re-installed the cutting edge of the strip stall after refinish with stainless steel equipment. A new external ELT antenna has been installed and the navigation antenna has been replaced with a new one. All control surfaces are balanced, checked by weight and balance, the change is defined insignificantly. All procedures and processes have been reviewed and approved. Signed, Robert D. Powell A No. 1267538499 FIREWALL FORWARD END REFURBISHMENT Following information from the engine log: Tachometer Time: 0 Total time with a new: 2097 hours of major repairs carried out on this Teledyne Continental Series 10 5520K Model Powerplant Serial Number 557440 at the factory specification according to teledyne Motors Continental Capital Repair Guide. Complete disassembly of all internal parts and components. All internal steel parts are magnafluxed, V.A.R. Crankshaft magnafluxed and ultrasound inspection performed by Buldoc Aviation Specialized Services Repair Station #KM5R993M. All six mic cylinders are checked for specifications and restored to the original factory tolerances using the NU-CHROME process by Harrison Engine Services Inc. Repair Station #NOLR2R988K. The fuel injection system is repaired including a new engine-driven mechanical fuel pump by the Aircraft Accessories Certified Repair Station - RV3R829L. The following new parts WERE INSTALLED (NEW INTERNAL ENGINE PARTS) SIX SA530658 Rod Bushings / SIX-SA641951 Exhaust Valve Guide / SIX-SA643776 Consumption Valve Guide / SIX SA646895 Oil Seals / Eight-SA350998sha Crank Bushftings/ Twelve-SA Four- SA643525-101 30261-37 Pins/TWO-SA-630261-38 Counter-Weight Pins / Twelve-SA630826 Rod Bearings / Twelve-SA629340 Rod Bolts / Twelve-SA628109 Nuts Rod / Twelve-AN38125-10 Keys / One-SA-535661 Camshaft / One-555756-8 Key / Six SA-637837 Exhaust Rollers / Six-SA539988 Intake Valves/ Twelve SA629117-1 Roto Reel / Twelve SA631521/ Twelve SA-637837 Valve Springs / Six SA-628488 ltaken Lifters / Six SA646277 Lifts / SA666666588-A1 Crankshaft Main bearing set / Six SA648013 Pistons (Set)I Six SA52 01SC2 Piston Rings (Set)/ Twelve 652541 Cylinder Base Nuts / Thirty-six 531001 Cylinder Base Nuts / One l0-823674-1 Teledyne Continental Motors Ignition Wiring Harness/ Twelve-Six 531001 Cylinder BaseE Spark Plugs. Cleaned and tested oil coolers/bent, inspected and resealed oil pump/collected power plant with all new sets of pads, seals and hoses according to Teledyne Continental Motors Capital Repair Guide. Overhaul starter / overhaul of the alterator / Overhaul left and right Magneto assembly / Installed (OBA) New Magneto Cam Assembly PV 10-400166-4/ Installed new magneto Seals (OBA) P.N. l0-48944/ Executed with AD No 82-20-1 Bendix Magneto Impulse Couplers on (BOTH) Magnetos/ Next Due at 500 Hours Tach Time/ All Engine Airworthiness Directives to date have been implemented. The engine is ready to return to service. THE ENGINE IS NOT PRE-OIL. END Signature: Signature: The leaders of the ACP #1428281. ADDITIONAL SERVICES FORWARD FIREWALL 1. This engine is installed on the N28013 Bellanca 17-30A S1N79-30955 after the O/H I.A.W. Bellanca Maintenance Guide. 2. Replaced all firewall hoses forward, (1 ea) oil, (6 ea) fuel, (1 ea) air, (5 ea) hydraulic, and (8 ea) duct hose. 3. C/W AD 96-12-22 Oil Filter Adapter Inspection. All safe because of the following on Tach 100.0 or the removal of the oil filter. 4. C/W AD 76-23-03 R1 Exhaust Inspection System. The tension set on AD should be next on Tach 100.0. 5. C/W AD 84-26-02 Paper induction air filter by replacement, which should be introduced next on Tach 500.0. 6. Two new polished exhaust stacks have been installed, P/N 201047-0 and P/N 201048-0. 7. Service engine with 12 qtsshell Aero 100 mineral oil and pre-oil engine 8. Magneto has been checked for up to 20.' 9. The test ran the engine, no leaks noted. I confirm that the aircraft was inspected in accordance with the annual inspection and it has been determined that it is in a state of air condition. Signature: Robert D. Powell IA 267538499. PROP MAGAZINE TACH: 0.0 T.T.: 2097.0 1. This prop is installed on the N28013 Bellanca 17-30A S/N79-30955 After O/H I.A.W. Bellanca Maintenance Guide. I confirm that the aircraft was inspected in accordance with the annual inspection and it has been determined that it is in a state of air condition. Signature: Robert D. Powell IA267538499 AIRCRAFT INSTRUMENT PANEL REFURBISHMENT All instruments, avionics, switches, etc., removed from the dashboard. Remote dashboard and control wheels to refine to the original new specification of parts. The dashboard was completely stripped to bare metal and upgraded to the original specification using approved materials. For this aircraft was used the original beige almond color with black silkscreen on the new aviation process. All new colored beige almond screws installed on the assembly. New switch frames, color code posters of numerous hardware as needed and various details like-new look. Installed all the tools after refinish as a new look. AlI avionics bench checked, aligned with the specification. The photovoltaic cells have been replaced in nav/coms. All avionics operations have been checked and reinstalled in aircraft. Re-installed S-TEC 60 Pitch stabilization system after factory maintenance. Installed updated (to the original specification coverage) control yokes (2) and installed a new center piece Bellanca emblem. Re-installed push-to-talk control wheel, map light, autopilot shutdown and electric finish switch after refinished for that mark a new condition. A new zero-time TACHOMETER, the new internally lit VERTICAL SPEED INDICATOR part #7040 Serial No. 281630, has been installed. Both communication antennas removed the Transponder antenna. A new large ground aircraft has been installed. The new Com antenna C 1-122 (bent whip) has been installed and a new coaxial cable number one com has been installed. A new ground has been installed on the lower/bottom of the fuselage and a second new Com C1-122 antenna (bent whip) has been installed. whip). The new coaxial for the number two com, installed a new ground aircraft and installed a new coaxial cable for the transponder. A new C1-105 transponder antenna has been installed. The DME antenna has been removed and replaced with the C1-l05 antenna. New static lines and fittings for the pitot/static system have been installed. All necessary checks and operational checks of all systems have been carried out. All operations are well checked. Return to service. The end. ADDITIONAL INTERIOR/ INSTRUMENT PANEL ITEMS REPLACED WITH NEW Vernier control of the throttle cable and handle Vernier control propeller control cable and handles (blue for the new requirement) Vernier control cable control mix and handle New 6 probe E.G.T. Gauge New 6 probe E.G.T. Gauge selector switch (6 position switch) New selector fuel switch, indicator and housing 1. They removed the vacuum track from the plane and installed a new factory track. The test started the plane, all the checks are good. 2. The altimener tests and inspection required by FAR 91 .411 were performed, and it was found to correspond to the FAR 43 Annex E at an altitude of 20,000 feet at altitude Part Number: 503 SP-P44 Serial number 17931. 3. The static system of the aircraft required by FAR 91. 411 were executed and found satisfactory Tach 0.0 4. The ATC Transponder and Inspection tests required by FAR 91.413 were performed and found to be in line with the FAR 43 Annex E and F. Make: Collins Model TDR-950 Serial Number: 25085. Details of these inspections are archived at this repair station in accordance with our WO-1621. AIRCRAFT INTERIOR REFURBISHMENT REMOVED COMPLETE INTERIOR for a complete revamp to the factory's original specification, pattern and stitch configuration using Bellanca, lnc. plant of new materials in accordance with the Federal Aviation Regulations 25.853 requirements for burns testing. All window frames have been removed, paint stripped and refined at the plant the original color code is reinstalled with new equipment including new stainless steel screws. All new factory green shades of plexiglass have been installed, including a new windshield, a pilot ventilation window with a new weather lane vent. Prior to the installation of the windshield stripped and improved both windshield fuselage braces for the original semi-glossy black and installed two new control marks. Two new lids with glare, covered with authentic black bark (dark brown) suede skin, have been installed. New screens of glareshield vents have been installed. The vertical compass appearance is refined. Removed cockpit floorboards and luggage floorboards, remove all lower insulation, carefully cleaned and reinstalled all new bottom covered foam insulation Carefully vacuumed and evacuated The fuselage cavity of any debris is cleaned and replaced with any belly insulation as required stripped all doork and steel pipes, including the luggage doorjamb, refined to correct the color, installed all new polished aluminum door slabs (provided that Inc.), new equipment and a spring hinge of the luggage door. A new strip of luggage doors has been installed. A new cockpit door has been installed under the pressure of the door seal in the STC SA2511NM installation instructions (see 337 Form in aircraft records). A new cockpit door has been installed at the sliding door. A new Chrome kit has been installed for the new Bellanca aircraft production, including sunvisor fittings and equipment, and new chrome hooks for cargo grids (only ten). A new cargo network has been installed. The interior has been renovated with the following Bellanca, Inc. plant new materials. This includes four head seats, four seats and seat backs, four side panels, a general luggage compartment design, a headliner, a carpet with additional top mats, matching rear seat pockets and two luggage door pockets. The rear seat, corresponding to the cushions of the decorator. Materials are: Headliner, Bellanca LP710 Sand Beige Puma Body cloth, Bellanca LL259 Maple Lynx. Vinyl finish, imitation of bellanca Mocha Eclipse leather. Carpet, Bellana Urine Eclipse with Moca Eclipse tying. Statement of compliance with federal aviation regulations in aviation documents. New appropriate seat belts and two new rear-appropriate shoulder strap Aero Fabricators, W.O. #0413067. Reinstalled matching front seat inertia) shoulder straps. Installed a new Bellanca, Inc. matching Cora 'brown' leather pilot operating directory with brass equipment and new content in clear plastic lamination pages. Installed a new Bellanca, lnc matching Bark Brown leather three rings binder with brass equipment. Content includes new logs for this repair and all aircraft records with new ones, including all magazines (original set). All updated information in the plastic laminated three-page ring relating to applicable airworthiness directives, etc. installed a new Electra-Voice microphone and bracket. A new tug-bar has been installed. A new fuel spill. A new fire extinguisher H3R Halon Firefighting Protection Aircraft used only, according to the project (F.A.A. approved) All ventilation controls, thermal control, internal lighting and four intercom system operations seats are tested approved for return to service. Signed by AP's Jesse D. Bono #216569990. 1979 Bellanka Super Viking 17-30A Serial #79-30955 Registration #N28013 Main Exterior: White First Color Finish: Burnt Orange Secondary Color Finish: Beige Color Interior: Mocco Eclipse Headliner: Sandy Beige Puma Glareshield: Black Bark (Dark Brown) Suede Leather / Factory New Vinyl Trim: Mocha Eclipse Fabric: Maple Lynx / New Carpet Factory: Mocha Eclipse / Factory New Tool Group: Almonds / Factory New Glass Hue: Green / Windshield and All Side Windows / Plant New General Aircraft Time With New: 2097 Hours Total Time From The New Tachometer: Zero - Now 42 Hours Total Time With Propeller Overhaul: Zero - Now 42 Hours Annual Status Inspection Including Airiness Worth Directive Directive Updated with Sale Aircraft Always Hangars Before This Service No Damage History STANDARD EQUIPMENT Electrical Expansion System Transfers Courtesy Dome Light Landing Gear Warning System Fully Illuminated Panel with Rheostats Stall Warning Systems Pilot Map Lights Landing and Taxi Lights Fun Electric System with Switches Nav Lights Heavy Duty 12 Volt Battery Strobe Lights 60 Amp Alternator 12 Volt Position Fuel Boost Emergency Locator Transmitter True Airspeed Indicator Recording Tachometer Sensitive Heighter Manifold Pressure Gauge Vertical Fuel Indicator Indicator Fuel Sensor Outside Air Temperature Sensor Fuel Sensor Grope- Continuous Reading Artificial Horizon Temperature Oil Sensor Direction Gyro Pressure Lap Belt for all seats Steerable Nose Wheel Driver Storm Window Door Ash Trays Towing Bar Double Lift Trim , cabin doors and luggage door locks of single fuel Selector Cleveland Wheels Double Pressure Drive Brake Sump Drain System Parking Brake Oil Fast Drainage Throttle and Mix FACTORY INSTALLED AIRFRAME OPTIONS Three Blade Propeller Golf Club / Ski Pipe Retainer Fifteen gallons fuselage auxiliary fuel tank (83 gallons in total) Co-pilot Brake Wheel Doors Auxiliary Power Vessel Electric Trim Control Microphone Switch (Push-to-Talk) Right side of the microphone Jacks Electrovoice Microphones (2) Right side of the microphone Reclining front seat front seat front seat and rear inertia Harness Shoulder Luggage Storage Pockets suede Glare shield cover left side of the Sun Visor tinted Plexiglas Height reporting High Altitude Altimeter (United Instruments) W T Strobe Light System Proflite Operating Group / Deluxe Interior Lighting Deluxe Internal Package and Lighting Wheel Map Light Chrome Kit Cleveland Wheels and Brakes Six Probe EGT Engine Analyzer Vertical Compass Pitot Heat Built in ELT Cowl Flaps Towing Bar Radio Master Switch Pure AVIONICS PACKAGE - Fun Collins Digital Microline Collins AMR-350 Audio Panel with Three Light Markers Beacon Collins VHF-251 Transiver Collins VHF-251 Transiver Collins Receiver Collins VIR-351 Receiver Collins IND-350 VOR / Localizer Indicator Collins IND-351 VOR / Localizer / Glideslope Indicator Collins GLS-350 Glideslope Receiver Collins RCR-650-ADF Receiver Collins IND-650-ADF Indicator Collins ANT-650-ADF DME Transyver Collins IND-650-ADF Indicator Collins ANT-451 DME Antenna Collins TDR-9S0 Transponder with Height Reading Collins ANS-351 RNAV Eight Waypoint Memory Navigation Pc Collins ANS-351 351 351 THE LIGHT PS Engineering Four Place Intercom Avionics Master dual position Electric watch GPS II Morrow Apollo Model 8002 AUTOPILOT Century IIB upgraded to S-TEC Pitch / Stabilization system equivalent to S-TEC 60-2 Autopilot, which includes height hold plus vertical speed Select, Glideslope couple, VOR/LOC/BACKCOURSE plus GPS connection. 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