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Guidelines for minimizing risks during inspection and maintenance.
Details component time limits, overhaul, and replacement schedules.
Procedures and schedules for routine maintenance inspections.
Specific inspection requirements for critical items at 1000-hour intervals.
Step-by-step guide to weighing the aircraft and calculating the C of G.
Instructions on how to properly level the aircraft for accurate measurements.
Provides standard and special torque values and measuring techniques.
Details the DC generation system, including battery, master relay, and alternator.
Describes the flight control system, including overview and tolerances.
Details maintenance procedures for ailerons, rudder, elevator, and trim tabs.
Covers refueling, defueling, and vapor hazard reduction.
Procedures for main landing gear and mounting clamp removal/installation.
Instructions for tail wheel fork, tail wheel, and brake system maintenance.
Describes the magnetic compass and turn and bank indicator.
Details damage classification and criteria for component repair or replacement.
Outlines repair methods for composite, sandwich, laminate, spar, steel, and painted parts.
Instructions for wing removal and installation.
Describes the MTV-12-B-C/183-17e propeller and its operation.
Describes the engine installed in the EXTRA 200 and its control systems.
Lists engine specifications, accessories, and operational controls.
Details the inverted oil system, its hoses, and fittings.
General| Manufacturer | Extra Flugzeugbau |
|---|---|
| Role | Aerobatic aircraft |
| Crew | 1 |
| Capacity | 1 passenger |
| G limits | +10/-10 |
| Wing area | 10.44 m² |
| Engine | Lycoming AEIO-360 |
| Power | 200 hp |
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