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Related Manuals for Flugzeugbau Extra 300
Summary of Contents for Flugzeugbau Extra 300
- Page 1 Chapter 05 Time Limits/Maintenance Checks...
- Page 2 Table of Contents 05-00-00 GENERAL 05-10-00 TIME LIMIT COMPONENTS 05-20-00 SCHEDULED MAINTENANCE CHECKS 05-50-00 UNSCHEDULED MAINTENANCE CHECKS...
- Page 3 05-00-00 GENERAL N O T E For working with checklists refer to Chapter 02-20-03. D A N G E R Do not rotate the propeller nor allow any person to stay in the propeller operating area when performing an in- spection or check with the master switch "ON"...
- Page 4 05-10-00 TIME LIMIT COMPONENTS 05-10-01 General 05-10-02 Overhaul Schedule Item Overhaul Engine * refer to latest issue of (Textron Lycoming) Manufacturer´s Service Bulletin together with Engine accessories engine Magneto (Slick) Double magnetos (Bendix) Propeller (MT-Propeller) Governer (Woodward) All other components on Condition...
- Page 5 05-10-03 Recommended Replacement Times Item Replace Battery ** on the recommendation 2 years ** of the manufacturer (Sonnenschein) Batteries of the ELT 2 years ** (Pointer) Wheels on Condition (Cleveland, Parker) Tires on Condition Fuel, oil & brake hoses after first 7 years, (Aeroquip) then 5 years Seat belts...
- Page 6 05-20-00 SCHEDULED MAINTENANCE CHECKS 05-20-01 General 05-20-02 25 Hour Inspection - Engine 05-20-03 25 Hour Inspection - Aircraft...
- Page 7 1. Root Rib Aileron 2. Root Elevator 3. Root Horizontal Stabilizer 4. TrimTab (3 Holes) 5. Stall Warn Transducer 6. Lower Root Rudder Fin 7. Lower Root Rudder Horn 8. Wheel Fairing 9. Nose Ribs Aileron (Hinge Gaps) Drain and Vent Holes Figure 1...
- Page 8 Lubrication Chart 25 hours Figure 2...
- Page 9 Lubrication Chart 50 hours Figure 3...
- Page 10 Lubrication Chart 100 hours Figure 4...
- Page 11 05-20-04 Maintenance Checks Schedule Operational Checks...
- Page 12 Propeller Ground magneto primary circuit before D A N G E R working on propeller refer to MT-Propeller Service Bulletin No. 1...
- Page 13 Engine compartment Ground magneto primary circuit before D A N G E R working on engine 1 at 10 and 25 hours and then each 25 hours 2 at 10 and 25 hours 3 each 500 hours...
- Page 14 1 each 300 hours 2 each 25 hours 3 each 400 hours...
- Page 15 TCM/Bendix magnetos Slick magnetos 1 each 500 hours 2 at engine overhaul and at the expiration of 4 years 3 each 1000 hours 4 together with engine...
- Page 16 1 clean at least every 90 days...
- Page 17 Fuselage 1 refer to Woodward Service Bulletin No. 33580 refer to Lycoming Service Instruction No. 1009...
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Page 18: Flight Controls
Fuel system Flight controls 1 each 25 hours... - Page 19 Landing gear Fairings:...
- Page 20 Wheels Tires...
- Page 21 Brake system Tail-wheel landing gear...
- Page 22 a) Standard: Full-swivel tailwheel b) Optional: Steerable tailwheel Wing...
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Page 23: Electrical System
Stabilizer Instruments Electrical system Annual, each twelve calendar month... - Page 24 05-20-05 Significant Items Inspection 1000 flight in addition Wing Leading edge Main spar section Auxiliary spar section Spar carry-through...
- Page 25 Wing trailing edge Root and Tip Aileron Surface general Control system...
- Page 26 Vertical Stabilizer Leading edge Front spar section Rear spar section Root and Tip Rudder...
- Page 27 Horizontal Stabilizer Leading edge Front spar section Rear spar section Spar carry-through Root and Tip Elevator...
- Page 28 Surface general Fuselage Flight controls...
- Page 29 Main landing gear Tail-wheel landing gear Standard: Full-swivel tail-wheel Optional: Steerable tail-wheel...
- Page 30 Engine compartment Hardware...
- Page 31 Surface general...
- Page 32 05-50-00 UNSCHEDULED MAINTENANCE CHECKS I M P O R T A N T In case of abnormal events or any exceedance of given limitations (load factor, never exceed speed, etc.) the manufacturer has to be contacted to find appropriate maintenance procedures. Therefore the procedures de- scribed in the following could be subjected to changes.
- Page 33 Landing gear Control surfaces Engine...
- Page 34 05-50-03 Engine Fire 05-50-04 Lightning Strike...
- Page 35 05-50-05 Flightline Inspections...
- Page 36 General Min 3,5mm (1/8") (Min 6,0mm (1/4") Rudder Pedal with newly installed rudder cables) Safety Wire Hole Safety Stop Minimum Clearance Check Figure 5 Coning Check Figure 6 2 as required...