
Rules Governing Model Aviation Competition in the United States
Academy of Model Aeronautics
5151 East Memorial Drive
Muncie, Indiana 47302-9252
For events 201, 202, 204, 205, 206, 207, 208, 209, 210, 211, 213, 214, 215, 216, 220.
5.1. A rise-off-ground (R.O.G.) Indoor Model shall have a takeoff gear that permits it to take off from the ground or floor under its own power. The takeoff gear must be strong enough to support the model in a normal attitude while at rest and permit it to take off without damage, nosing over, or striking a wing tip. When one wheel is used, skids or similar devices shall be required to keep the model upright and in a normal attitude and to prevent any part other than the takeoff gear from touching the ground, floor, or runway. At the moment of release, the model must be held in such a manner that at least one (1) or more points are resting on the ground, floor, or runway.
5.2. The minimum diameter of wheel(s) for rise-off-ground models shall be: stick, 0.50 inches (1.27 centimeters); cabin, 0.75 inches (1.905 centimeters). The wheel(s) shall rotate freely.
12.1. The height of the building is defined as the vertical distance from the floor to the highest point at which a circle of 15 meters (in diameter) can be inscribed, below the primary structure of the building.
12.2. In FAI Indoor (F1D), a record flight shall be the best single flight of a series of six (6) flights.
12.3. If an indoor site contains a reasonably permanent structure with an elevated upper surface larger than 15 meters in its smallest dimension, flights may be launched from this surface provided:
a. The added elevation of the launch surface does not change the official ceiling category of the flight.
b. The model must land no lower than the elevation of the launch point. If the model lands below the launch point, the flight shall be recorded as zero time or score.
15.1. All supporting and stabilizing surface (wing, stabilizer, and rudder) can be covered with any commercially available solid material such as plastic film or paper. Microfilm is not allowed.
15.2. Propellers may be carved from a solid block, formed from sheet stock, or be built-up and covered with any commercially available solid material such as plastic film or paper. Microfilm is not allowed.
19.2. Characteristics.
19.2.1. The Easy B model shall be a monoplane covered with any commercially available material sold in sheet form. Microfilm is not allowed.
19.2.2. The maximum projected wingspan is 18 inches (45.72 centimeters).
19.2.3. The maximum wing chord allowed is three (3) inches (7.62 centimeters).
19.2.4. The motor stick shall be solid and made from a single piece of wood. The tail boom shall either be an extension of the motor stick or a separate piece of solid wood. It is permissible to use splints of wood less than 3/8 inch (0.953 centimeters) long, attached directly to the original wood, to repair structural damage to the tail boom and motor stick.
19.2.5. There are no restrictions on model length.
19.2.6. There shall be no minimum weight restrictions on the model.
19.2.7. Stabilizer area shall not exceed 50 percent of the projected wing area.
19.2.8. There shall be no bracing on the model except that which consists entirely of solid wood. The use of any material except wood for bracing on Easy B models shall not be acceptable. The intent of the Easy B rules is that all structures shall be constructed entirely from wood, using adhesives solely to assemble the structure.
19.2.9. Propeller. The propeller blades shall be constructed entirely from wood, with the following exception: Special novice or beginner events can be set up for local competition by permitting the use of plastic commercial propellers, provided advance notice is given in contest announcements. It is not acceptable to use any material other than wood for the propeller blades and spars, one (1) wire for the propeller shaft, and adhesive for assembly. No gadgets of any kind (such as variable pitch or variable diameter mechanisms) are permitted as part of the propeller. Propeller hubs which permit blade replacement and manual pitch adjustment are acceptable.
19.2.10. The structural framework of the Easy B model shall be entirely of wood with adhesive for assembly only. Reinforcement utilizing boron, carbon fiber, Kevlar(tm), or any other non-wood substance is not allowed. Tissue or thread wrap at the thrust bearing and rear hook is acceptable.
19.2.11. It is prohibited to use any scheme, device, or mechanism which affects the rate of energy release from the rubber motor, except for propeller blade flare or deformation.
20.2. Characteristics.
20.2.1. Airframe weight without rubber shall be four (4) grams minimum.
20.2.2. The overall length of the model, measured without the prop, shall not exceed 20 inches (50.8 centimeters).
20.2.3. The fuselage must meet the following requirements.
20.2.3.1. It must support and enclose a single rubber motor. No rigid internal structures such as motor sticks allowed.
20.2.3.2. The external structural members of the fuselage must include a theoretical box measuring 2.5 inches X four (4) inches X two (2) inches (6.35 X 10.16 X 5.08 centimeters), or larger.
20.2.3.3. The fuselage must include a windshield of two (2) square inches minimum area and a window on each side of one (1) square inch minimum; windshield and windows to be cellophane or similar transparent material. If transparent covering is used on the fuselage, then the windshield and windows must be outlined in a contrasting color.
20.2.4. The propeller shall be all wood except for shaft and hook for rubber attachment, with fixed pitch and directly driven by the rubber motor.
20.2.5. The wing shall be a monoplane with 20 inches (50.8 centimeters) maximum projected span and four (4) inches (10.16 centimeters) maximum chord.
20.2.6. The horizontal stabilizer shall be a monoplane with 12 inches (30.48 centimeters) maximum projected span and 3.5 inches (8.89 centimeters) maximum chord.
20.2.7. Wood bracing of wind and horizontal stabilizer is allowed.
20.2.8. The landing gear shall be fixed and rigid with at least two (2) freely turning wheels of one (1)) inch (2.54 centimeters) minimum diameter; the landing gear shall be able to support the airplane at rest on the takeoff area.
20.2.9. All covering of the model except for the windows shall be paper or commercially available plastic; no microfilm allowed.
20.2.10. Scoring. All flights shall rise off the ground from at least a two-point starting position; the best single flight of an unlimited number of official flights shall count. At the discretion of the Contest Director, the best single flight of five (5) official flight shall be counted.
21.2. Pennyplane. For
event 207.
21.2.1. The model shall weigh at least 0.109 ounces (3.10 grams) without the rubber motor.
21.2.2. The overall length, including the propeller, shall not exceed 20 inches (50.8 centimeters). The length is to be measured by placing the prop blade leading edges against a vertical plane. The rear-most part of the model must not extend beyond a line parallel to the vertical plane and 20 inches from it.
21.2.3. The projected wingspan, measured perpendicular to the motor stick, shall not exceed 18 inches (45.72 centimeters).
21.2.4. The distance from the front of the thrust bearing to the rear motor hook shall not exceed 10 inches (25.4 centimeters).21.2.5. A single direct drive (ungeared) rubber motor and propeller shall be used to power the model.
21.2.6. The rubber motor shall not be enclosed.
21.3. Limited Pennyplane. For event
208.
21.3.1. All rules applicable to Pennyplane shall apply to Limited Pennyplane, with the following exceptions applying specifically to Limited Pennyplane.
21.3.2. The wing chord shall not exceed five (5) inches (12.70 centimeters).
21.3.3. The dimensions of the horizontal stabilizer shall not exceed four (4) inches chord by 12 inches span (10.16 x 30.48 centimeters).
21.3.4. The motor stick shall be solid and made from a single piece of wood. (The tail boom may be a separate solid piece.)
21.3.5. The propeller diameter shall not exceed 12 inches (30.48 centimeters).
21.3.6. No gadgets of any kind are permitted on the model (i.e., variable pitch props, automatic incidence changing mechanisms, etc.).
21.3.7. Limited Pennyplane is limited to monoplane models.
22.2. Intent of Rule. This is an event to promote indoor flying of realistic propeller-driven, rubber-powered models of a size and complexity which are suitable for small buildings and limited skills. It also allows fanciful designs, for which no full-size counterpart exists, to be flown.
22.3. Charisma Judging. A "charisma factor" of 1.00 through 1.20 will be awarded each airplane before flight, based on the purpose stated above. The assignment of charisma factor will be made with all the models grouped together so they can be ranked and compared. There is no reason to award either a 1.00 or a 1.20 score to any of the models in a particular competition. These numbers represent the limits of the range to be used. The judge is encouraged to assign values with at least two (2) significant numbers to the right of the decimal point to fully use the factor to differentiate among the models being judged. This factor will be awarded with whatever weighting the appointed charisma judge sees fit and is not to be the subject of protest after judging. Argument about the charisma scoring will be considered unsportsmanlike conduct with penalties provided in this book.
22.4. Flight Scoring. Five (5) official flights will be allowed with the sum of the best two (2), in seconds, being used as flight score. The final score will be the flight score multiplied by the charisma factor. Flight begins when the model is released for an unassisted takeoff and ends when the model next touches the floor, or is prevented from forward flight by an obstruction for more than 10 seconds. The ten-second rule will be applied in the same way as in endurance events. A flight of less than 20 seconds may be considered an attempt or an official flight (at the flier's option, to be exercised immediately) and two (2) attempts will be allowed for each of five (5) official flights. Any flight in which there is accidental contact with steering apparatus, people, or other models may be considered no-flight (at the flier's option, to be exercised immediately) with neither an official flight nor an attempt being recorded. A flight in which the model does not take off or is assisted in takeoff is listed as a zero (0) time attempt. A bounce caused by roughness of the takeoff surface or a liftoff with a stall and no climb is not to be considered a takeoff. Hand launching may be used if, in the opinion of the Contest Director, floor surface conditions are likely to prevent a significant number of the entries from rising off the ground.
22.5. Timing. All flights must begin with release for unassisted takeoff from a position in which the model is resting on the takeoff (landing) gear with no push allowed. If the Flier's hand moves in the direction of flight on release, this will be interpreted as a push and a zero (0) time attempt will be charged.
22.6. Specifications.
22.6.1. Maximum projected wingspan shall not exceed 16 inches (40.64 centimeters).
22.6.2. Maximum wing chord (measured parallel to the direction of flight) shall not exceed three (3) inches (7.62 centimeters).
22.6.3. The diameter of the propeller(s) shall not exceed six (6) inches (15.24 centimeters).
22.6.4. The length of the model, excluding the propeller(s), but including the thrust bearing(s), shall not exceed 14 inches (35.56 centimeters). This measurement will be made in the direction of flight and will include surfaces which extend beyond the thrust bearing or fuselage end because of a sweep or unusual mounting.
22.6.5. The fuselage structure must include a box which has minimum dimensions of 1.5 inches x 2.5 inches x 3.0 inches (3.81 centimeters x 6.35 centimeters x 7.62 centimeters). The width (the horizontal dimension perpendicular to the line of flight) of the fuselage shall not exceed three (3) inches. The box must be enclosed within the fuselage structure and must be covered so as to restrict free air movement through the box. Normal sag of the framework between supports caused by the tension of the covering will not be considered as a violation of this rule.
22.6.6. The fuselage structure must be built-up so that the longitudinal members (the longerons) support the forces produced by the rubber motor. A solid or hollow motor stick with a lightweight structure added on is not acceptable.
22.6.7. The fuselage must have a transparent windshield and side windows of at least one (1) square inch (6.45 centimeters) area each. An open cockpit design need not have side windows, but the windshield must meet the one (1) square inch rule (6.45 square centimeters) and must stand at least 3/4 inch (1.905 centimeters) above the top of the fuselage.
22.6.8. The model must have at least two (2) wheels of at least 3/4 inch (1.905 centimeters) diameter which rotate freely and support the model for takeoff and landing. The inside surfaces of the wheels must be separated by at least 2.5 inches (6.35 centimeters) in the direction of the axis of the wheels.
22.6.9. All flying surfaces must be covered on both sides or must be solid material with a thickness of at least 1/16 inch at the maximum point in each chordwise element.
22.6.10. To qualify as a monoplane, the total projected area of the secondary horizontal surface(s), excluding that inside the fuselage, shall not exceed 24 square inches (152.8 square centimeters). This may be a conventional stabilizer and/or a canard surface. Secondary horizontal surfaces exceeding this total area limit will be considered to be additional wings.
22.6.11. The airframe, excluding the rubber motor(s), shall weigh at least seven (7) grams for a monoplane or 10 grams for others. These weights may be increased at the discretion of the Contest Director if advanced notice is given to contestants. No trim tabs or other appendages which result in specified dimensions being exceeded, will be allowed.
22.7. Only one (1) entry per contestant is allowed.
23.1. Models must be built from published plans or kits which represent real, man-carrying aircraft. Kit materials may be replaced in kind. That is, hardwood parts will be replaced by hardwood, balsa by balsa, etc.
23.2. Size of plans may be reduced or enlarged if wood sizes are in proportion to the original.
23.3. All surfaces must be covered on both sides with tissue paper. No condenser paper or films are allowed. Uncovered solid materials may be used.
23.4. Models must take off unassisted for official flights.
23.5. Any flight in which the model is airborne for more than ten (10) seconds is official.
23.6. Two (2) attempts may be used for each of five (5) official flights.
23.7. Timing starts when the model is released and terminates when the model next touches the floor or comes to rest after takeoff. The ten second hang-up rule as described in Section 9, Timing of Flights, will be used.
23.8. No flight score (in whole seconds) will exceed the total of Craftsman and Fidelity points.
23.9. Each contestant is limited to one entry. Models will be judged before they are flown. Plans and instructions from which the model was built must be submitted. Up to 60 points will be awarded for fidelity of the model to the plans and/or printed instructions from which it was built. Any changes in the structure or finish will result in a penalty of one (1) or two (2) points, depending on the nature of the change. If the change is made in several places, the penalty will be assessed for each place. In cases of disagreement between the plans and instructions, the builder must select which of the options he will use and highlight it on the plans or instruction sheet which he submits to the judges. In cases where the plans and/or instructions do not show how something is done, the builder is free to improvise. Also, see 23.11 and 23.14.
23.10. Up to 40 points will be awarded for craftsmanship, based on workmanship and finish. Visible rough finish, poorly fitted joints, wrinkled and puckered tissue, poorly located or attached decorations should all result in one (1) or two (2) penalty points for each infraction. Surfaces which are warped or tissue which is puckered because of inadequate or poorly designed structure should be penalized lightly. Also, see items 23.12 and 23.13 below.
23.11. Nose block and rear rubber attachment method may be altered to allow stretch winding, insertion of a winding tube and easy hook up without penalty.
23.12. Tissue type and color are optional, but control outlines and registration numbers (even if made up) must be used.
23.13. Decorations or paper panels which are supposed to be cut from the plan and glued to the model must be so done, but they may be reproduced on similar weight paper and cut out to preserve the plan.
23.14. Propeller and thrust bearing may be altered from the plan without penalty.
23.15. Final score is the sum of the best tow (2) flight scores plus Craftsmanship plus Fidelity.
24.2. The Mini-Stick model shall be a monoplane covered with any commercially available material sold in sheet form. Microfilm is not allowed.
24.3. The maximum projected wingspan shall be seven (7") inches.
24.4. The maximum wing chord shall be two and one-half (2-1/2") inches.
24.5. The maximum length (from front of nose bearing to front of rear motor hook) shall be five (5") inches.
24.6. The maximum length from front of nose bearing to rear most part of model shall be ten (10") inches.
24.7. The projected area of the stabilizer shall not exceed 50 percent of the projected area of the wing.
24.8. The maximum diameter of the propeller shall be seven (7") inches. The propeller shall be constructed of wood. Wire shafts are permitted. Hubs that allow blade replacement and/or manual pitch adjustment are allowed. Mechanisms that cause variable pitch and/or variable diameter of propellers while in flight shall not be allowed. (Natural flexing and flaring of wooden blades is allowed.)
24.9. The minimum overall weight of the model (without motor) shall be 0.015 ounce.
24.10. Construction is to be primarily of wood, with adhesives used only for joining. Tissue and/or thread is permitted for wrapping bearings, hooks, and for making sockets, if desired. Boron, carbon fiber, Kevlar, and fine wire bracing are not permitted.
24.11. Mechanisms that restrict the torque available to the propeller are not allowed.
25.2. An Experimental Autogiro model is supported in flight solely by the action of vanes or rotor(s) which rotate freely on an approximately vertical axis. No fixed wing(s) may be used.
25.3. The area of the lifting surface is defined as the swept disc area of the vanes or rotor(s). This area is computed by multiplying 3.14 times the square of the radius of the rotor or rotors. If more than one (1) rotor is used, the lifting surface is the sum of the individual swept disc areas.
25.4. Each individual vane or rotor blade must have an aspect ratio no less than 4:1. The aspect ratio is computed by dividing the rotor diameter by twice the average vane width.
25.5. The total area of all horizontal stabilizing surfaces shall not exceed 10 percent of the total lifting surface. No limit is placed on the area of vertical stabilizing surface(s). If a "V-Tail" configuration is used, the horizontal lifting surface is defined as the projected area of the V-tail surface.
25.6. Scoring for Experimental Autogiros shall conform to the provisions of sections 9 and 10 of the AMA Indoor Rubber rules.
25.7. The intent of this rule is to encourage experimental development of wingless Autogiros.
For events 212, 218, 219.
1. Applicability. All pertinent AMA regulations (see sections titled Sanctioned Competition, Records, Selection of Champions, and General) shall be applicable, except as specified below.
2. General. An Indoor glider is a non-powered model aircraft designed to fly indoors.
3. Classes. The following classes shall be recognized for competition and National Records:
a. Hand-Launched Glider.
b. Standard Class Catapult Glider.
c. Unlimited Class Catapult Glider.
4. Size of Supporting Surfaces. The projected area of a supporting or stabilizing surface is the area seen when looking directly down on the surface. Supporting surface area enclosed in a fuselage or stick shall not be considered as wing area. Projected area of horizontal stabilizing surface(s) in excess of 50 percent of the projected area of the supporting surface (wing area) shall be considered as wing area.
a. Hand-Launched Glider. The projected area of the supporting surface(s) must not be more than 100 square inches.
b. Standard Class Catapult Glider. The projected wing span must not exceed 12 inches. The projected wing chord shall not exceed three (3) inches. The area of the horizontal stabilizing surface(s) shall not exceed 50 percent of the projected wing area. Standard class is limited to monoplanes.
c. Unlimited Class Catapult Glider. The projected area of the supporting surface(s) must not be more than 100 square inches.
5. Construction. All surfaces shall remain fixed except for changes of camber or incidence due to natural flexing of the surfaces. Folding wings and mechanically actuated incidence changes are strictly prohibited.
6. Launching. Launching shall be appropriate to the class of model. In all cases, the launch shall be made with force sufficient to cause the glider to immediately gain altitude equal to three (3) times the flier's height or half the available ceiling height, whichever is less. The model shall not be launched from a height greater than the flier's normal reach above the floor.
a. Hand-Launching. The model shall be released into flight directly from the hands of the contestant, without other assistance.
b. Catapult Launching. The model is launched by stretching elastic band(s) between the hands of the contestant, with one end(s) firmly attached to a launching handle. The handle shall consist of a rigid dowel or similar device, with the elastic band(s) firmly attached.
The launching handle (including the attachments for the elastic) shall not exceed six (6) inches in length, measured along the longest dimension. The handle may use padding or contoured grips for flier comfort. There is no limit to the length or sizes of the elastic bands. All launching apparatus must remain firmly attached to either the handle or the model during launch. There is no limit to the number of launching handles a contestant may use to complete his/her flights.
7. Number of Gliders. Each contestant shall be permitted a maximum of three (3) gliders per contest. The three (3) gliders used may be of different design.
8. Official Flight. All flights are official flights, regardless of duration. Unofficial flights are not recognized. A flight during which any part is dropped shall be declared an official flight with zero (0) time.
9. Number of Flights. Each contestant shall be allowed a total of nine (9) official flights.
10. Scoring of Flights. Scoring time shall be the total elapsed time of the best two (2) of not more than nine (9) official flights. Flight duration shall be scored in tenths of seconds, with hundredths of a second dropped. Example: 65.17 seconds shall be recorded as 65.1 seconds.
11. Flying for Record. The same ceiling height categories and specifications apply as for Indoor Rubber models.