Van's Aircraft RV-12iS Flight Training Supplement

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Date: 09/08/20
Revision: 4
FLIGHT TRAINING SUPPLEMENT
RV-12iS Flight Training Supplement
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Do you have a question about the RV-12iS and is the answer not in the manual?

Questions and answers

Joe Bacon
April 8, 2025

Does lane A provide control of both ignition for the cylinders by itself?

1 comments:
Mr. Anderson
April 9, 2025

Yes. In the RV-12iS, Lane A (as part of the dual electronic engine management system) controls one of the redundant electronic ignitions. Each lane can control ignition for all cylinders. If one lane fails, the other can assume control of all critical functions, including ignition.

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Summary of Contents for Van's Aircraft RV-12iS

  • Page 1 Date: 09/08/20 Revision: 4 FLIGHT TRAINING SUPPLEMENT RV-12iS Flight Training Supplement...
  • Page 2: Revision Summary

    Page 6-6 removed regulator manufacturer from text. Page 6-5 replaced GTN 650 with GTN 650Xi Section 05/07/20 Page 6-7 replaced GMC 307 with GMC 507 Page 6-8 replaced GTN 650 with GTN 650Xi and GMC 307 with GMC 507 RV-12iS Flight Training Supplement...
  • Page 3: Table Of Contents

    SECT X CRUISE 10-1 SECT XI MANEUVERING FLIGHT 11-1 SECT XII DESCENT 12-1 SECT XIII LANDING 13-1 SECT XIV SHUT DOWN 14-1 SECT XV EMERGENCY PROCEDURES 15-1 SECT XVI GROUND HANDLING 16-1 APPENDIX 1 TRAINING SYLLABUS A1-1 RV-12iS Flight Training Supplement...
  • Page 4 Date: 09/08/20 Revision: 4 THIS PAGE INTENTIONALLY LEFT BLANK RV-12iS Flight Training Supplement...
  • Page 5: Sect

    This Flight Training Supplement (FTS) was carefully prepared by the test pilots, flight instructors, and engineers of Van's Aircraft - the manufacturer of the RV-12iS. The FTS has been prepared with the goal of enabling the new pilot or a pilot transitioning from another aircraft to quickly and efficiently learn about features and characteristics specific to the RV- 12iS.
  • Page 6 Date: 09/08/20 Revision: 4 Recommended Links 1. General information about Van's Aircraft as well as drawing and manual revisions: https://www.vansaircraft.com/ 2. General information about the Sport Pilot rule and Light Sport Aircraft: https://www.eaa.org/en/eaa/aviation-communities-and-interests/light-sport-aircraft 3. ACK ELT: http://ackavionics.com 4. Dynon Avionics: https://dynonavionics.com/...
  • Page 7 Most of the literally hundreds of features which comprise the overall RV-12iS package have been determined in the design stage.
  • Page 8 This limited the span of the horizontal tail surface to 8 ft. The limited tail span requires that the RV-12iS use a long fuselage placing the tail surfaces well aft for good control authority.
  • Page 9 “droop” and simultaneously perform the function of ailerons and flaps. The flap action on the RV-12iS is electrically operated. The stabilator and rudder are connected to the controls by pull cables. The stabilator trim tab is driven by a DC motor.
  • Page 10 Date: 09/08/20 Revision: 4 THIS PAGE INTENTIONALLY LEFT BLANK RV-12iS Flight Training Supplement...
  • Page 11 BASICS OF LOADING THE RV-12iS The RV-12iS design places the pilot and passenger forward of the CG and baggage/other payload aft of the CG. Thus, the most-forward loading condition occurs with the heaviest possible pilot and passenger weights combined with minimum fuel and no baggage.
  • Page 12 For Rotax 912ULS powered aircraft, the fuel pump is located between the tank and the gascolator. First run the fuel pump for 2 mins, then drain the gascolator to remove contaminants and water. Note the water may be mixed with the fuel (as shown in the pre-flight section below). RV-12iS Flight Training Supplement...
  • Page 13 SECTION IV PRE-FLIGHT INSPECTION INDEX GENERAL CABIN LEFT MAIN LANDING GEAR 4-13 LEFT WING 4-14 FUSELAGE (LEFT SIDE) 4-16 EMPENNAGE 4-17 FUSELAGE (RIGHT SIDE) 4-20 RIGHT WING 4-22 RIGHT MAIN LANDING GEAR 4-25 NOSE SECTION 4-26 GENERAL RV-12iS Flight Training Supplement...
  • Page 14 Date: 09/08/20 Revision: 4 RV-12iS Flight Training Supplement...
  • Page 15 Date: 09/08/20 Revision: 4 RV-12iS Flight Training Supplement...
  • Page 16 CANOPY LATCHED POSITION LIFT HANDLE CAUTION: Take care unlocking the controls in gusty conditions. In gusty conditions, a canopy left in the open position must be latched with the Support Plate Canopy Latch. RV-12iS Flight Training Supplement Support Plate Canopy Latch...
  • Page 17 Collapse Rudder Lock then stow in baggage area. CAUTION: Take care unlocking the controls in gusty conditions. In gusty conditions, the canopy left in the open position must be latched with the Support Plate Canopy Latch. RV-12iS Flight Training Supplement...
  • Page 18 WARNING Continue sampling fuel until there are no contaminants detected. WARNING During high ambient temperature conditions, run the fuel pump for 5 mins to flush the fuel lines and minimize the potential for vapor lock. RV-12iS Flight Training Supplement...
  • Page 19 If the battery voltage is low, proceed to engine start and then let the engine run for at least 5 mins at 2000 rpm to flush the fuel system RV-12iS Flight Training Supplement...
  • Page 20 Date: 09/08/20 Revision: 4 CABIN (continued) • Master switch – ON • (If Garmin GTR-200 Installed Check Radio – ON) • Avionics – ON MASTER SWITCH AVIONICS SWITCH RV-12iS Flight Training Supplement...
  • Page 21 450lb resting on the c-channel and the seat back brace is one possible method of restraining the baggage from forward movement. Baggage should not be loaded so high in the baggage area that it may come forward. RV-12iS Flight Training Supplement...
  • Page 22 Wheel Pant (If Installed) – CONDITION CHECK • Wheel Chocks – REMOVE NOTE Properly inflated tire has no contact between the outer portion of tread and pavement BRAKE PADS VERIFY NO INTACT BRAKE FLUID AXLE NUT LEAKAGE COTTER RV-12iS Flight Training Supplement 4-10...
  • Page 23 This is usually discovered by hearing a clicking noise. If this is the case, refer to the Maintenance Manual for corrective action. Excessive fore and aft play in the left wing may also DOWN render the EFIS AOA indications inaccurate. RV-12iS Flight Training Supplement 4-11...
  • Page 24 Verify that it hits a definite stop at both ends of its travel and that there is no binding or limiting friction. FLAPERON MOVEMENT TRAILING EDGE DOWN FLAPERON MOVEMENT TRAILING OUTBD HINGE EDGE UP BRACKET BOLT RV-12iS Flight Training Supplement 4-12...
  • Page 25 • Controls – CONNECTED Verify that the tab on the inboard end of the flaperon FLAPERON fully engaged into the slot in TAB FULLY the actuator when the wing ENGAGED IN was installed. ACTUATOR SLOT RV-12iS Flight Training Supplement 4-13...
  • Page 26 Vertical Stabilizer – CHECK condition and security Look at vertical stabilizer in general, look for dents (Particularly dents in the leading edge), wrinkles, missing or loose rivets, missing or loose screws. Confirm solid attachment to the fuselage. RV-12iS Flight Training Supplement 4-14...
  • Page 27 Verify clearance between anti-servo tab pushrod in fully up position and rudder in any position. ANTI-SERVO TAB PUSHROD ATTACH BOLT RV-12iS Flight Training Supplement 4-15...
  • Page 28 FULL LEFT VERIFY LOWER HINGE BOLT RUDDER MOVEMENT FULL RIGHT RUDDER HINGE BOLT • Look into the slot for the anti-servo pushrod and check: Lower Rudder Hinge Bolt Elevator Cable Bolts Rudder Cable Bolts Elevator Trim RV-12iS Flight Training Supplement 4-16...
  • Page 29 • Comm. Antenna - CHECK condition & security Verify that the ADS-B & comm. antennas are securely attached and have not been damaged. Verify that the skin surrounding the antennas is not bent or wrinkled. RV-12iS Flight Training Supplement 4-17...
  • Page 30 Date: 09/08/20 Revision: 4 FUSELAGE (RIGHT SIDE) (continued) • Fuel Vent Line- CLEAR FUEL VENT AIR LINE FUEL VENT LINE • Fuel Vent Air Line - CLEAR • Fuel Cap - SECURE WHEN LATCHED RV-12iS Flight Training Supplement 4-18...
  • Page 31 Date: 09/08/20 Revision: 4 FUSELAGE (RIGHT SIDE) (continued) • Controls - CONNECTED RIGHT WING • Flaperon - HINGE BRACKET ATTACHMENT Verify that the outboard, mid, and inboard flaperon hinge bracket bolts are installed RV-12iS Flight Training Supplement 4-19...
  • Page 32 • Flaperon – CONDITION Look at flaperon in general, look for dents (particularly dents in the trailing edge), wrinkles, missing or loose rivets. RV-12iS Flight Training Supplement 4-20...
  • Page 33 If this is the case refer to the Maintenance Manual for corrective action. • Tie-Down – UNTIE the tie-down rope/chain, REMOVE eye bolt if desired. Ensure eye bolt is secured in the wing if not removed. RV-12iS Flight Training Supplement 4-21...
  • Page 34 Brake – CHECK condition, NO leakage • Axle Nut – CHECK cotter pin installation • Wheel Bearings – SHAKE top of tire left and right • Wheel Pant (If Installed) – CONDITION CHECK • Wheel Chocks – REMOVE RV-12iS Flight Training Supplement 4-22...
  • Page 35 Date: 09/08/20 Revision: 4 NOSE SECTION • Transponder Antenna – CHECK condition & security • Muffler – CHECK condition, security of attachment RV-12iS Flight Training Supplement 4-23...
  • Page 36 4. Use the start key to turn the propeller for 10 seconds 5. MASTER OFF 6. Check the oil level 7. Replace the cap from the oil tank • Cowl Door - CLOSED • Nose Landing Gear – • CHECK attachment to fuselage RV-12iS Flight Training Supplement 4-24...
  • Page 37 FINAL WALKAROUND • Fuel Sample – CHECK until no more fuel/ water mixture is present. • CHECK quick drain valve for leakage. PITOT TUBE LEFT AIR INLET RIGHT AIR INLET OIL & COOLANT RADIATORS WHEELPANT RV-12iS Flight Training Supplement 4-25...
  • Page 38 Date: 09/08/20 Revision: 4 THIS PAGE INTENTIONALLY LEFT BLANK RV-12iS Flight Training Supplement 4-26...
  • Page 39: Cabin Overview

    CANOPY CLOSED SAFETY SWITCH 5-16 GENERAL This section covers the features of the RV-12iS cabin. See POH Section 7 and RV-12 FTS Section VI for labeled diagrams of the instrument panel, stick grips and center console. RV-12iS Flight Training Supplement...
  • Page 40 Exiting the aircraft is accomplished by performing the reverse of one of the above entry methods. (OPTIONAL) CABIN LIGHT ROLL BAR NON-SKID CABIN DECK PASSENGER BOARDING STEP RESTRAINTS HEADSET PLUGS (ON SEAT PAN NOT VISABE) SPAR PIN RV-12iS Flight Training Supplement...
  • Page 41 The seat back position and recline angle can be adjusted independently of each other. SEAT BACK ADJUSTMENT GUIDES SEAT BACK BRACE SEAT BACK SLIDE PIN PIN PLATE RV-12iS Flight Training Supplement...
  • Page 42 BELT BELT HEADSET, AUDIO INPUT Standard GA headset plugs are located next to the seats, along the outboard side between the seat bottom cushion and the exterior wall of the airplane. HEADSET PLUGS (MIC AND PHONES) RV-12iS Flight Training Supplement...
  • Page 43 Left Flaperon: DOWN Left Flaperon: DOWN Left Flaperon: UP Left Flaperon: DOWN Right Flaperon: UP Right Flaperon: UP Right Flaperon: UP Right Flaperon: DOWN Stabilator: UP Stabilator: UP Stabilator: DOWN Stabilator: DOWN RV-12iS Flight Training Supplement...
  • Page 44 Independent left and right brakes on the main gear are used to steer the aircraft at low taxi speeds and may be used to turn the aircraft around a small turning radius. LEFT RIGHT BRAKE BRAKE PEDAL PEDAL RUDDER CONTROL NOSE TO THE LEFT NOSE TO THE RIGHT RUDDER RV-12iS Flight Training Supplement...
  • Page 45 Date: 09/08/20 Revision: 4 TRIM PITCH DOWN Trim is adjusted using a momentary- TRIM contact switches located on the stick grip. See Section VI for further information about trim operation. PITCH TRIM D-180 RV-12iS Flight Training Supplement...
  • Page 46 CONTROL POWER mode is engaged when the throttle position is advanced beyond approximately 97%. The RV-12iS is equipped with an “eco stop” which allows the THROTTLE throttle position to be advanced up to approximately 97% (i.e. the upper limit of ECO mode). To use the “eco stop”, apply leftward pressure to the throttle handle while advancing the throttle.
  • Page 47 The heated air continues into the engine compartment, or into the cabin depending on the position of the cabin heat control knob. CABIN HEAT (PILOT SIDE) RV-12iS Flight Training Supplement...
  • Page 48 On a G3X or SkyView system, if the RPM is set to a speed greater than 3700 RPM while the canopy is open, such as during the run-up or take-off roll, an audio warning as well as an on-screen warning will be annunciated. CANOPY SWITCH RV-12iS Flight Training Supplement 5-10...
  • Page 49 As you read this section, please reference the electrical systems schematics found in POH Section 7. RV-12iS ELECTRICAL SYSTEM THEORY The RV-12iS electrical system is designed to minimize the workload of the pilot while keeping cost and weight to reasonable minimums.
  • Page 50 Date: 09/08/20 Revision: 4 ELECTRICAL SWITCHES & KNOBS RV-12iS Flight Training Supplement...
  • Page 51: Electrical System

    MASTER SWITCH: This switch connects the battery to the main electrical bus (the power source for the rest of the electrical system) via a solenoid. When the master switch is on the EFIS(s) will automatically start. RV-12iS Flight Training Supplement...
  • Page 52 ELT REMOTE: The ELT remote switch has on “ON” switch that should be activated in an emergency and a test switch that may be used during the first 5 mins of every hour to test the function of the ELT. AVIONICS SWITCH: This switch controls power to the transponder and the installed COM radio. RV-12iS Flight Training Supplement...
  • Page 53 Main Bus to Bus A and Bus B of the engine. This turns on the engine computers (Lane A and Lane B), provides engine sensor data to the EFIS and provides power to start the engine. The RV-12iS automatically detects that the master switch has been turned on and that the engine is not running (Bus A voltage will be below 13.7...
  • Page 54 The fuse panel is located directly on the center console. Replacement fuses are stowed in a special holder underneath the instrument panel on the pilot side of the aircraft. The fuse holder is retained using a hook-and-loop tape fastener. RV-12iS Flight Training Supplement...
  • Page 55 The user's guide can be downloaded - see Section 1 Links for internet location. AITHRE CARBON MONOXIDE DETECTOR If the optional Aithre carbon monoxide detector is installed, the carbon monoxide level detected in the cockpit will be displayed on the PFD. RV-12iS Flight Training Supplement...
  • Page 56 Date: 09/08/20 Revision: 4 RV-12iS Flight Training Supplement...
  • Page 57: Sect

    RPM is low while stationary. During taxi operations with the canopy in the open position, the canopy must be latched with the Support Plate Canopy Latch. See POH Checklist BEFORE TAKEOFF RUN UP See POH Checklist RV-12iS Flight Training Supplement...
  • Page 58 Date: 09/08/20 Revision: 4 THIS PAGE INTENTIONALLY LEFT BLANK RV-12iS Flight Training Supplement...
  • Page 59: Takeoff

    The RV-12iS when loaded at or near its maximum weight is limited primarily in its take-off distance. Stated another way, if an RV-12iS can take off from any given runway it can, when properly flown, easily land on that same runway.
  • Page 60 Date: 09/08/20 Revision: 4 THIS PAGE INTENTIONALLY LEFT BLANK RV-12iS Flight Training Supplement...
  • Page 61: Climb

    See POH Checklist During high temperature days, be mindful of engine oil temperature. If temperature approaches the caution range, lower the nose to decrease climb rate, allowing the airspeed to increase and improve cooling. RV-12iS Flight Training Supplement...
  • Page 62 Date: 09/08/20 Revision: 4 THIS PAGE INTENTIONALLY LEFT BLANK RV-12iS Flight Training Supplement...
  • Page 63 Cruising at max-endurance indicated airspeed makes sense if the aircraft is being used as an observation platform or for some other mission where time spent aloft is of greater concern than the number of miles covered. RV-12iS Flight Training Supplement 10-1...
  • Page 64 Date: 09/08/20 Revision: 4 THIS PAGE INTENTIONALLY LEFT BLANK RV-12iS Flight Training Supplement 10-2...
  • Page 65 To turn off the ESP function, touch to select the AP annunciator bar at the top of the Flight Instruments area of the EFIS screen. When the Automatic Flight Control System screen appears, touch and select ESP to turn it off. RV-12iS Flight Training Supplement 11-1...
  • Page 66 Strive to maintain constant airspeed throughout the turn and when airspeed increases above V . reduce the amount of bank before attempting to increase pitch. Maintain attitude by visual reference to the horizon with only very quick glances at the EFIS to verify consistent altitude. RV-12iS Flight Training Supplement 11-2...
  • Page 67 Date: 09/08/20 Revision: 4 Repeat the above exercise except perform the turn to the right. Repeat the above exercise except use 55-60° of bank. Repeat the above exercise except perform the turn to the left. RV-12iS Flight Training Supplement 11-3...
  • Page 68 Date: 09/08/20 Revision: 4 THIS PAGE INTENTIONALLY LEFT BLANK RV-12iS Flight Training Supplement 12-1...
  • Page 69: Descent

    80 KIAS and place the aircraft in a 50-60 degree bank descending spiral. The loss of vertical lift allows for a more rapid descent without building-up excess speed. Clear the engine every 1000’ with a short application of power. RV-12iS Flight Training Supplement 12-2...
  • Page 70 Date: 09/08/20 Revision: 4 THIS PAGE INTENTIONALLY LEFT BLANK RV-12iS Flight Training Supplement 12-3...
  • Page 71: Landing

    To avoid unnecessary nose gear loads, it is especially important that the nose wheel is held off the ground and lowered gently to the runway after speed has diminished. RV-12iS Flight Training Supplement 13-1...
  • Page 72 When calibrated, AOA indicators provide a three-color visual display of the AOA in addition to an aural tone. This tone will change intensity in correlation to proximity of Critical AOA. Refer to your EFIS pilots guide for specific details regarding the specific AoA device installed in your aircraft. RV-12iS Flight Training Supplement 13-2...
  • Page 73: Shut Down

    Place the flaps in the full up position and secure the control stick in the full aft position using the pilot lap belt. Use the tow bar to secure and lock the rudder controls in place as shown in Section IV. RV-12iS Flight Training Supplement 14-1...
  • Page 74 Date: 09/08/20 Revision: 4 THIS PAGE INTENTIONALLY LEFT BLANK RV-12iS Flight Training Supplement 14-1...
  • Page 75 All airspeeds in this section are indicated knots airspeeds (KIAS) unless stated otherwise. ABNORMAL ENGINE INDICATIONS See POH FIRE ENGINE FIRE DURING START See POH ENGINE FIRE IN FLIGHT See POH ELECTRICAL FIRE See POH RV-12iS Flight Training Supplement 15-1...
  • Page 76 7 kts above stall speed. An AOA indicator system is installed in the RV-12iS. It uses an AOA pressure port located on the underside of the left wing near the leading edge. (Pages 4-3 & 4-12). As the angle of attack increases, the AOA port is exposed to more direct airflow.
  • Page 77 Do not lower flaps when ice is present, as doing so changes airflow over the tail and can induce a stabilator stall. Also, the stall warning horn may cease to function or function falsely because of ice formation on the leading edge of the wing. See POH Checklist RV-12iS Flight Training Supplement 15-3...
  • Page 78 This procedure assumes landing with a complete stabilator control failure (locked in the up & down movement axis) Besides the stabilator, there are three other forms of pitch control in the RV-12iS: Flaperons, Trim tab and Throttle. Flap extension and retraction commands will result in normal pitch changes, but will be the reverse of conditioned reflexes for normal control stick commanded pitch changes.
  • Page 79 At or above approximately 15 kts, adequate steering (except in crosswinds) can be maintained with aerodynamic rudder control.At lower speeds the RV-12iS relies at least in part on differential braking for ground steering. On any landing the pilot has two basic goals: a) to bring the airplane to a stop and b) to keep it moving straight enough to remain on the runway.
  • Page 80 Date: 09/08/20 Revision: 4 THIS PAGE INTENTIONALLY LEFT BLANK RV-12iS Flight Training Supplement 16-1...
  • Page 81 Remove dirt and insects from painted surfaces with water alone and if necessary with a mild detergent or automotive paint cleaner. Oil stains, exhaust stains and grime on the lower fuselage skin can be removed with a cold detergent. RV-12iS Flight Training Supplement 16-2...
  • Page 82 2. Withdraw each of the fuselage pins only enough to release the right wing spar. 3. Remove the right wing and set aside. 4. Remove both of the fuselage pins. 5. Remove the left wing and set aside. INSTALLATION Installation procedure is reverse of the removal procedure RV-12iS Flight Training Supplement 16-3...
  • Page 83: Appendix

    Appendix 1: RV-12iS Training Syllabus Training in the RV-12iS. The goal of this syllabus is to provide Flight Instructors with an efficient system to train new RV-12iS pilots regardless of previous flight experience and proficiency. The RV-12iS presents the pilot with some unfamiliar items not common in other production-type airplanes.
  • Page 84 1. Clear the area with two 90º turns 2. Reduce power, while maintaining altitude until airspeed is about 55 kts. 3. With wings level, add take off power while increasing nose-up attitude by approximately 15°. RV-12iS Flight Training Supplement A1-2...
  • Page 85 Once the pilot has demonstrated proficiency, the instructor can opt to practice other emergencies like inadvertent IMC 180º turn and/or other IR maneuvers. Other topics: Basic Autopilot and Navigation functions demonstration if aircraft is so equipped. Standards: Pilots should demonstrate a minimum of Private Pilot Standards throughout maneuvers during this training. RV-12iS Flight Training Supplement A1-3...
  • Page 86 Date: 09/08/20 Revision: 4 THIS PAGE INTENTIONALLY LEFT BLANK RV-12iS Flight Training Supplement A1-4...
  • Page 87 Date: 09/08/20 Revision: 4 FLIGHT TRAINING SUPPLEMENT RV-12iS Flight Training Supplement FRONT COVER...
  • Page 88 Date: 09/08/20 Revision: 4 THIS PAGE INTENTIONALLY LEFT BLANK RV-12iS Flight Training Supplement FRONT COVER...
  • Page 89 Date: 09/08/20 Revision: 4 RV-12iS Flight Training Supplement REAR COVER...
  • Page 90 Date: 09/08/20 Revision: 4 THIS PAGE INTENTIONALLY LEFT BLANK RV-12iS Flight Training Supplement REAR COVER...

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