The Complete Multi-Engine Pilot

Oxygen ............................................................................................................. 29 Jets.................................................................................................................... 30 Summary .......................................................................................................... 30 Review Questions ............................................................................................. 31 Contents SAMPLE iv Contents 3 Planning and Performance 33 Weight and Balance Calculations ...................................................................... 33 Zero-Fuel Weight .............................................................................................. 34 Lateral Balance ................................................................................................. 38 Performance Planning ...................................................................................... 38 Minimum Controllable Airspeed ...................................................................... 40 Minimum Controllable Airspeed on the Ground .............................................. 42 Minimum Safe Single-Engine Speed ................................................................. 42 Best Angle and Best Rate-of-Climb Speeds........................................................ 42 Landing Gear Extension and Operating Speeds ................................................. 43 Engine-Out Climb Speeds ................................................................................. 43 Maneuvering Speed, Normal Operating Speed, and Never-Exceed Speed .......... 44 More Important V-Speeds ................................................................................. 44 Performance Airspeeds Versus Weight .............................................................. 44 Using Performance Charts ................................................................................ 44 Review Questions ............................................................................................. 52 4 Preflight Preparation 53 The Preflight Inspection .................................................................................... 53 Taxiing.............................................................................................................. 53 Student and Instructor Relationship .................................................................. 54 Passenger Briefing ............................................................................................. 54 Preflight Runup................................................................................................. 54 Last Thoughts…................................................................................................ 54 Review Questions ............................................................................................. 55 5 Takeoff and Departure 57 Engine Failure on Takeoff ................................................................................. 57 Calculating Climb Rates Before Takeoff ............................................................ 59 The Takeoff Roll ................................................................................................ 60 Engine Fails! ..................................................................................................... 61 Cleaning Up the Airplane ................................................................................. 62 “Abnormal” Takeoffs ......................................................................................... 63 Review Questions ............................................................................................. 65 6 Cruising Flight 67 The Cruise Checklist ......................................................................................... 67 Service and Absolute Ceilings ........................................................................... 69 Engine Failure During Cruise Flight ................................................................. 70 Drift Down ....................................................................................................... 71 Review Questions ............................................................................................. 72 7 Descent, Approach, and Landing 73 Descent Planning .............................................................................................. 73 Beginning the Descent ...................................................................................... 73 Leveling Off ...................................................................................................... 74 On Final ........................................................................................................... 74 Landing Distance .............................................................................................. 75 Getting It Stopped ............................................................................................. 75 SAMPLE Contents v Single-Engine Approach and Landing ............................................................... 76 Landing with a Propeller Feathered ................................................................... 77 Review Questions ............................................................................................. 78 8 Energy Management 79 Importance ....................................................................................................... 79 Basics of an Airplane Energy System ................................................................. 79 Managing Energy.............................................................................................. 79 Roles of the Flight Controls ............................................................................... 80 Basic Rules of Energy Control ........................................................................... 81 Managing Risks and Errors ............................................................................... 81 Review Questions ............................................................................................. 83 9 Preparing for the Checkride 85 Certificates and Documents .............................................................................. 85 Airplane Systems .............................................................................................. 85 Normal Procedures ........................................................................................... 86 Determining Performance and Flight Planning ................................................. 86 Minimum Equipment List................................................................................. 86 Flight Principles: Engine Inoperative................................................................. 86 Ground Operations ........................................................................................... 87 Normal and Crosswind Takeoffs and Climbs ..................................................... 87 Maximum Performance Takeoffs and Climbs .................................................... 88 Instrument Flight .............................................................................................. 88 Slow Flight and Stalls ........................................................................................ 88 Spins ................................................................................................................. 88 Steep Turns ....................................................................................................... 89 Drag Demonstration ......................................................................................... 89 VMC Demonstration ......................................................................................... 89 System and Equipment Malfunctions ................................................................ 90 Balked Landing ................................................................................................. 92 Normal and Crosswind Approaches and Landings ............................................ 92 Maximum Performance Approach and Landing ................................................ 92 Appendix A: Multi-Engine Rating Syllabus ....................................................93 Appendix B: Written Exam for Multi-Engine Checkout .............................. 103 Appendix C: Answers to Review Questions ................................................ 109 Appendix D: Further Study in FAA Source Material.................................... 113 Glossary ........................................................................................................... 183 Index ................................................................................................................ 187 SAMPLE viii Art Blanster’s six-passenger single-engine airplane is sleek, fast, and equipped with the latest in navigation equipment, but it is uncomfortably close to its maxi- mum gross takeoff weight when he loads it with his business associates and the equipment they need to make a sales demonstration in a distant city. A multi- engine airplane will give Art the load-carrying capa- bility that he needs. Adding “Multi-Engine Land” to his certificate is a business necessity. Paula Forsham’s flying club has six singles and a twin, and she is checked out in every one of the sin- gle-engine airplanes. Six months ago, a vacuum pump failure in one of them resulted in a descent through clouds using needle, ball, and airspeed, and just last week a broken alternator belt caused a total electrical failure. Paula is aware that a twin’s redundant vacuum and electrical systems will tip the odds in her favor. Pat Manley is 21 and has already logged 1,400 hours in single-engine airplanes as an instructor and charter pilot. He wants to put a multi-engine Airline Transport Pilot certificate in his wallet when he turns 23, and he knows that the more twin time he has in his log, the better his chances with a commuter or major airline will be. For Pat, getting a twin rating is a smart career move. Each of these pilots accepts the fact that getting a multi-engine rating will involve additional costs, but they all feel the advantages outweigh the cost factor. Each pilot will rationalize the decision to upgrade in his or her own way, but there is no denying that having Multi-Engine Land added to a pilot’s certificate pro- vides the extra pride of accomplishment that goes with stepping up to a higher skill level. Paula, Pat, and Art are ready to take on a new challenge—are you? MULTI-ENGINE TRAINING The FAA does not require you to log a minimum num- ber of hours of instruction before the multi-engine checkride. The flight check is a demonstration of proficiency, and your instructor will sign the recom- mendation form when he or she feels you are ready. During training, you will probably spend an hour or two doing airwork such as slow flight, approaches to stalls, and steep turns, to develop a sense of how an airplane with more of its mass off-center behaves. Pat- tern work will consist of normal takeoffs and landings as well as short- and soft-field takeoffs and landings. Then the emphasis will shift to emergencies, both at altitude and close to the surface. You can hone some of the required skills in a good multi-engine simulator, at a considerable reduction in cost and total time. My definition of a “good” multi- engine aviation training device (FAA-speak for what light-plane folks call simulators) is one that replicates the changes in control pressures that occur when an engine fails—most pilot reactions to emergency situ- ations are based on rudder pressure. Although skill levels of pilots and instructors vary, figure that five hours is a questionable short course, and that twenty hours of airplane time is overkill. Ground-training device time will shorten the amount of airplane time required. No FAA Knowledge Exam is required for the multi- engine rating, but you can expect to be grilled on your trainer’s performance numbers and operational sys- tems by your instructor, by the examiner who gives you the checkride, and by anyone from whom you rent a similar twin. Thorough knowledge of any multi- engine airplane’s systems is required. Introduction to Twins SAMPLE Introduction to Twins ix 14 CFR 61.129(b)(4) has been changed to allow a pilot to log solo time (“performing the duties of pilot-in-command”) in a twin when the right seat is occupied by an appropriately rated instructor. This change was driven by the insurance industry, which would not provide coverage for a twin flown solo by a pilot not rated in the aircraft. This is an outline of what you are getting into, as far as flying goes. Now let’s talk about this book. Isn’t it true that almost all of your one-on-one edu- cation as a pilot took place before you received your Private Pilot certificate, when new information and experiences were a part of every flight lesson? Except for being checked out in different singles, have you had many opportunities to sit down with an instructor and go over how the aeronautical facts of life you learned as a student apply to larger, more powerful airplanes? As a multi-engine pilot, your safety and that of your passengers will depend on your full understanding of the aerodynamic laws that govern flight in a twin when one engine is not delivering power. This book is intended to serve as that one-on-one talk. Yes, there are dual systems, but they offer more vari- ables than you have been exposed to in single-engine airplanes. You need a thorough grasp of how these sys- tems work, what they can do for you, and how they are affected by an engine failure. This book will dig more deeply into systems than did your basic texts. What will the examiner look for on your check- ride? To what new experiences will your multi-engine instructor expose you? What new elements of flight planning will a multi-engine airplane require? We’ll go through each of these subjects together, with the goal of making you a knowledgeable multi-engine pilot. Other than having an extra engine, how does a twin differ from the airplanes you have been flying? We’ll discuss that first, with special attention to operating systems, then we will look into the planning consid- erations. From there, we will go into a normal takeoff and climb, cruise considerations, approach planning, and the landing. All-engine and engine-out proce- dures are discussed in each section. We’ll discuss the FAA Airman Certification Standards for the multi- engine rating and talk about how to prepare for each area of operation and task. From the earliest hours of your private pilot train- ing you were asked, “Where would you put it if the engine failed?” Your job was to find a suitable landing site within gliding distance, and you didn’t have to fight to control the airplane on the way down. When one engine quits on a twin, however, control is your paramount concern. That is why your training—and this book—will concentrate heavily on what to do if an engine fails, why the failure causes control problems, and how following the correct procedures will make the airplane easier to control. There will be review questions at the end of each chapter. They are meant for confirming your under- standing, not for preparing for a Knowledge Exam. THE MULTI-ENGINE INSTRUCTOR RATING A flight instructor with a multi-engine rating on his or her pilot certificate can add a multi-engine rating to his or her flight instructor certificate by taking a checkride with an FAA operations inspector or des- ignated examiner. No minimum training time is required, and there is no knowledge examination. However, the applicant must have logged at least 15 hours as pilot-in-command in the category and class of aircraft involved (multi-engine land or multi-engine sea). Additionally, before training a pilot in a specific make and model of multi-engine airplane, an MEI must have logged 5 hours as pilot-in-command in that make and model. That is, if you get your MEI in a Duchess you must log 5 hours of Seneca II time before giving multi-engine instruction in a Seneca II. This is not a nit-picky requirement—manufacturers make changes in systems and procedures between models, and you cannot assume that what worked with twin A will work with twin B. IMPORTANT V-SPEEDS AND DEFINITIONS As you begin your multi-engine training, you will be introduced to many important performance V-speeds and their definitions unique to multi-engine airplanes. Many of these speeds are specific to one-engine-inop- erative (OEI) operations. Below is a list of these impor- tant speeds and definitions that you will come across during your training. This list of V-speeds and the glossary in the back of book are good, quick references to look up the definition of a specific V-speed or term. VR Rotation speed—speed at which back pressure is applied to rotate the airplane to a takeoff attitude. SAMPLE x Introduction to Twins VLOF Lift-off speed—speed at which the airplane leaves the surface. (Note: Some manufacturers reference takeoff performance data to VR, others to VLOF.) VX Best angle of climb speed—speed at which the airplane gains the greatest altitude for a given distance of forward travel. VXSE Best angle of climb speed with OEI. VY Best rate of climb speed—speed at which the airplane gains the most altitude for a given unit of time. VYSE Best rate of climb speed with OEI. Marked with a blue radial line on most airspeed indicators. Above the single-engine absolute ceiling, VYSE yields the minimum rate of sink. VSSE Safe, intentional OEI speed—originally known as safe single-engine speed. It is the minimum speed to intentionally render the critical engine inoperative. VREF Reference landing speed—an airspeed used for final approach, which is normally 1.3 times VSO, the stall speed in the landing configuration. The pilot may adjust the approach speed for winds and gusty conditions by using VREF plus an additional number of units (e.g.,VREF + 5). VMC Minimum control speed with the critical engine inoperative—defined in 14 CFR §23.2135(c) as the calibrated airspeed at which, following the sudden critical loss of thrust, it is possible to maintain control of the airplane. VMC is typi- cally marked with a red radial line on most air- speed indicators Remember, specific V-speeds for the airplane you are flying can be found in the airplane flight manual (AFM) or pilot’s operating handbook (POH) and can vary with aircraft weight, configuration, and atmo- spheric conditions. SAMPLE 1 extra horses would, if summoned to action, provide either greater level flight speed or climb capability. As you climb to higher altitudes, and the power output of the engines decreases, the ability to climb also decreases. When rate of climb has decreased to 100 feet per minute, the airplane has reached its service ceiling. Figure 1-2 on the next page illustrates how total drag varies with airspeed. Its components are induced drag, which is greatest at low speed and diminishes as speed increases, and parasite drag, which is neg- ligible at low speed but increases with the square of airspeed. The minimum total drag point (the bottom of the curve) is very close to the single-engine best rate-of-climb speed, which is achieved, in this illus- tration, at 40% power. As you can see, there is plenty of excess power to the right of the minimum drag point as long as both engines are running. When the power of one engine is not available, however, only the power in the shaded portion of the graph is available. High density altitude Why does a multi-engine airplane need two engines? Because it won’t fly on one, that’s why. To expand on this statement, the significant factor is “pounds per horsepower,” which relates to the amount of weight a given engine can haul into the air at sea level on a standard day. If you want to lift more pounds, you must either install a larger engine or add an engine, and there are practical limits as to just how big a sin- gle-engine can be for a given airframe. Big engines require lots of room and a plentiful source of cooling air, which translates into a large cowling with equally large frontal area. That, in turn, adds drag, and pretty soon you defeat the original purpose. Often, the best solution is a second engine. WHY TWO ENGINES? The Piper Seneca (Figure 1-1) is an excellent example of a manufacturer adding a second engine to an exist- ing airframe. Its ancestor, the Cherokee Six, with a single 300-horsepower engine, is able to carry seven people and has capacious baggage compartments. The Seneca I (the original, non-turbocharged model) was a Cherokee Six airframe with two engines. It didn’t offer much in the way of additional useful load, but it did provide two-engine safety. Other examples of singles that became twins when they grew up are the Twin Comanche and the Baron. The gain that is achieved by adding an engine is in excess horsepower. Every airplane derives its ability to climb from excess horsepower; excess, that is, to the amount of power required to sustain level flight. You typically choose a cruise power setting which keeps power in reserve, ready for use when called upon, instead of pushing all of the levers full forward. Those CHAPTER 1 The Concept of Multi-Engine Flying Figure 1-1. Piper Seneca II SAMPLE 2 The Complete Multi-Engine Pilot or a “good” engine which, for one reason or another, is not putting out full rated power, will cause the shaded area to shrink. During the first hour or so of multi-engine train- ing, you and your instructor can perform an experi- ment that will prove how the excess horsepower pays off. Trim your aircraft to maintain level flight at its best rate-of-climb speed and record the power setting; then, without touching the throttle or trim wheel, pull back on the control yoke and wait. For a few moments, the kinetic energy of the airplane’s forward motion will allow it to climb—but it won’t last. Because the increased angle of attack adds to induced drag, the airspeed will slowly decrease and the airplane will begin to descend. After a few oscillations, it will sta- bilize at the original altitude. You have established the minimum power required to maintain altitude. Now go back to the original situation (trimmed for level flight at VY) and add power; the aircraft will climb as a result of power in excess of that required to sustain level flight. It should be apparent that if an engine fails, erasing one-half of the total power, there will be little excess power available for climbing. To prove how the loss of excess power hurts perfor- mance, repeat your earlier experiment, but this time trim to maintain the single-engine best rate-of-climb speed (VYSE , or the blue line on the airspeed indi- cator) in level flight. Pull one throttle back to zero thrust (about 12 inches of manifold pressure is a good approximation) and do whatever is necessary to the remaining engine to avoid losing altitude. You will find that the “good” engine is producing 75% power or more, and that pushing it up to maximum power may Figure 1-2. Drag vs. airspeed result in a very modest rate of climb. The effect of the loss of power in excess of that necessary for level flight will be obvious. Indeed, depending on density altitude and weight, your airplane might not climb at all. File that away in your memory bank for later reference. This is the concept of multi-engine flight—add a second engine, and as long as both are humming the same tune, you will have copious amounts of excess horsepower to convert into cruising speed or climb capability if temperature, pressure altitude, and weight are within reasonable limits. That’s the good news. The bad news is that your multi-engine flight train- ing will place disproportionate emphasis on engine failures—disproportionate, that is, to the chance that you would ever experience a total power loss on one engine. All instructors know that placing emphasis on the negative aspects of a subject is a poor teaching technique, and it is with reluctance that they devote more time to the hazards of multi-engine flight than to its positive aspects. What they know, and what you should read into their instruction and into this text, is that multi-engine airplanes can be controlled when only one engine is running if the pilot knows what to do, how to do it, and why it is being done—and has the presence of mind to do the right thing when the situa- tion demands it. When your friends show you statistics on multi-engine accidents, point out that there are no statistics on how many twins experienced problems but landed without incident. When both engines are purring in sweet harmony, a twin doesn’t fly any differently than any sleek single- engine retractable. If the single-engine of that retract- able quits, however, the failure does not create control problems. You have little choice but to find the safest, least expensive spot to put it down. A second engine provides you with options, depending on where you are when the failure occurs. Some wags have said that it takes you to the scene of the accident. Realistically, once you have gained control of the airplane after an engine failure, the odds are very much in your favor. The FAA doesn’t require that a multi-engine air- plane weighing less than 6,000 pounds be able to climb or even maintain altitude on one engine; its only requirement is that the plane be controllable as it grad- ually sinks earthward. When you hear the phrase “light twin,” remember that 6,000-pound limit. However, almost all light twins are able to climb at least mini- mally on one engine. The Champion Lancer, a fabric- covered, fixed-gear twin, is known for its inability to Total drag 100 50 40 Induced drag Parasite drag Drag Airspeed V SO V YSE Power required – HP SAMPLE Chapter 1 The Concept of Multi-Engine Flying 3 maintain altitude when one of its little engines quits. Airplanes heavier than 6,000 pounds (or which stall at a speed higher than 61 knots) must demonstrate the ability to climb on one engine at 5,000 feet above sea level, and that means either more horsepower or turbocharging. BEGINNING YOUR MULTI-ENGINE TRAINING When you first learned to fly, your relationship with your instructor was clear-cut; the instructor took over control of the airplane whenever a situation began to deteriorate. You were a novice, your instructor was a professional, and “I’ve got it!” was your signal to let go of everything. When you begin your multi-engine instruction, the situation will change. You are now an experienced pilot, and until your instructor decides it is time to begin failing engines, he or she will place responsibility for normal operations in your hands. Unfortunately, the airplane doesn’t know this com- fortable situation exists, and it may decide to test the reactions of the entire front-seat crew. From the first takeoff, then, there should be complete understanding of who is in charge of the airplane if something out of the ordinary occurs. There have been many incidents in which each pilot thought the other was in control, and just as many in which both pilots were trying to fly the airplane at the same time. Instructional flight has the highest rate of accidents after engine failure, and for good reason. One profi- cient pilot can handle an engine-out emergency alone, and a crew of two with specific emergency duties assigned can handle a failed engine without it turning into an accident. With an instructor and multi-engine student occupying the front seats, however, confusion can result. The instructor wants to see how far into a situation the student can go without losing control, and the student feels that the instructor will bail him or her out before things get dicey. Each occupant of a pilot seat should have a clear understanding of his or her responsibilities as the throttles are pushed forward. By now I hope that you are asking, “What is so different about having one of the engines fail on a multi-engine airplane?” The answer lies in some aerodynamic laws you are already aware of. WHAT HAPPENS WHEN AN ENGINE FAILS When you practiced steep turns as a student pilot, you learned that if one wing is moving faster than the other, the lift imbalance will cause the airplane to roll toward the slower wing; you called it “overbank- ing tendency” then. You also learned about P-factor, the force created by the descending propeller blade that causes left-turning tendency in single-engine air- planes. Your instructor admonished you to use rudder when rolling into a turn to offset the drag created by a downward-deflected aileron. All of these elements will be present as we consider the effect of engine failure. Basically, when an engine fails on a twin, its wing is no longer being pulled forward and the opposite wing begins to move faster; the resulting yaw develops a rolling moment toward the dead engine. P-factor comes into play as the pilot increases the pitch atti- tude to avoid losing altitude. Finally, the windmilling propeller on the ailing engine creates drag of much greater magnitude than a deflected aileron. Put all of these reactions together, and you can visualize why the airplane rolls and turns toward the failed engine, and why, if the pilot does not act quickly and correctly, the airplane might hit the ground in a steep bank or inverted. It doesn’t have to happen, and your training will give you confidence in your ability to handle such an emergency if your skills are kept sharp. In later chapters, we will go into detail about what to do and why you do it. MULTI-ENGINE AERODYNAMICS Figure 1-3 shows the forces at work when both engines are operating. There is no imbalance in either thrust or lift. The propellers on both engines rotate clockwise as seen from the cockpit, so the descending blades on the right side of the propeller discs are doing most of the work. However, note that the left engine’s descending blade is much closer to the centerline of the fuselage than is the descending blade on the right engine. If the right engine fails, the yawing force exerted by the left engine’s P-factor will be relatively small, as indicated by the little arrow. If the left engine fails, however, the force exerted by the right engine’s descending blade will be farther from the centerline and the yawing force will be much greater; the large arrow empha- sizes the difference. The left engine is called the critical SAMPLE 4 The Complete Multi-Engine Pilot exerted by the tug on the right wing, and the push on the tail’s right side provided by the third tug’s driver. Replace the two wing-tip tugs with engine thrust and the fuselage tug with a fully deflected rudder, and you can see why an airplane with one engine inoperative and its wings level is slipping toward the dead engine. The relative wind blows against the side of the fuselage and the resultant drag increase is significant. There is no way to bring the relative wind into alignment with the centerline of the fuselage as long as the wings are level. Get the airplane airborne, however, and a new sta- bilizing force becomes available: the horizontal com- ponent of lift that is developed when the wings are banked. On the left side of Figure 1-5, control surface deflection replaces the forces exerted by the tugs in Figure 1-4, and the resultant motion is indicated by the arrows. When the wings are level, a vertical lift vector is developed, and the magnitude of that vector is equal to the weight of the airplane. As you begin to roll the airplane, the vertical lift vector shrinks (and you must increase the angle of attack to maintain alti- tude), and a horizontal lift component is developed which increases in proportion to the angle of bank. At a 90-degree bank angle, there would be no vertical lift vector and the airplane would fall out of the sky. So much for reviewing turn dynamics. By bank- ing toward the good engine (Figure 1-5, right side) you can develop a horizontal lift vector that will, in effect, provide a correcting force so the airplane will fly forward without any appreciable degree of sideslip. engine; its failure would create the most control prob- lems for the pilot. The propellers on twins certificated overseas usu- ally rotate counterclockwise as seen from the pilot seat, so the situation is reversed—for those airplanes, the right engine is the critical engine. Many modern multi-engine airplanes have coun- ter-rotating propellers—the right engine’s propeller rotates counterclockwise, so that the descending blades of both engines are equidistant from the centerline and P-factor cancels out. There is no critical engine. This reduces, but does not eliminate, the problems associ- ated with controlling the airplane on one engine. To illustrate how an engine failure causes a yaw and roll toward the dead engine, first look at the top of Figure 1-4 in which the thrust developed by the engines is represented by airplane tugs. (Since airplane tugs can’t get much traction when airborne, the air- plane in the illustration is on the ramp and cannot be banked.) The forces on the wings are balanced, and the airplane moves forward in a straight line. However, if one tug loses a wheel and stops pulling, the force of the other tug pulling its wing forward will cause the airplane to turn toward the dead tug. If a third tug rushes to the rescue and pushes on the good tug side of the fuselage near the tail, the turning motion can be arrested. Imagine all of this activity taking place in the dead of winter with the ramp covered with ice; the airplane will continue to move straight down the taxiway, although its nose is pointed to the right of the direction of travel. This is the result of the force Figure 1-3. Yaw force due to P-factor Figure 1-4. Zero sideslip without banking SAMPLE Chapter 1 The Concept of Multi-Engine Flying 5 takeoff and initial climb, during cruise, or during the descent and approach to land. Figure 1-6 illustrates the use of a yaw string, taped to the nose of the airplane and free to stream with the relative wind. The string streams toward the good engine side with the wings level, and becomes aligned with the longitudinal axis when the airplane is banked into the good engine, graphically illustrat- ing zero sideslip. The last few paragraphs have talked about bank angle. Go back to page 4 and note the words “fully deflected rudder.” Never fail to push the rudder on the good engine side all the way to the firewall; if you don’t stop the nose from yawing toward the dead engine it will be impossible to control the resulting roll. You could, theoretically, bank steeply enough that the horizontal component of force would make rudder deflection unnecessary. Of course, at liftoff and initial climb speeds, it is not possible to maintain altitude if you bank that steeply. Note the position of the ball on each side of Figure 1-5. With the wings level and the airplane slipping toward the dead engine, trim- ming the ball into the center is the wrong answer. FAA experiments have shown that a pilot can lose control of the airplane at airspeeds as much as 15 knots higher than the minimum control speed marked on the airspeed indicator if the wings are level with the ball centered. Minimum control speed (VMC) will be discussed in detail in Chapter 3. To achieve the book VMC figure, you must establish a bank angle of at least 5 degrees toward the good engine and let the ball move about one-half diam- eter toward the good engine. In this situation, the ball acts as a bank indicator, not a slip/skid indicator. A 5-degree bank duplicates the conditions under which the manufacturer determined VMC, and its intent is to help you regain control after an engine failure. The 5-degree figure does not apply in real life, however. Bank as much as you have to in order to avoid loss of control. As bank angle approaches 10 degrees, climb performance is adversely affected, though, so when you have the airplane under control, you can reduce the bank angle until the ball is deflected halfway out of the center for best performance. That lays the theo- retical foundation for the actions you will take in an engine-out emergency. In later chapters, we will dis- cuss just what you should do if an engine fails during Figure 1-5. Horizontal component of lift provides force to correct sideslip Figure 1-6. Yaw string Wings level Banked toward good engine SAMPLE 6 The Complete Multi-Engine Pilot CENTERLINE THRUST The obvious answer to the problems presented by off-center thrust is to place the engines on the air- plane’s centerline. This is just what Cessna did with the 336/337 Skymaster, which made its debut in 1964. The in-line twin served in Vietnam as the U. S. Air Force O-2. They were last produced in 1980, having failed to excite enough interest to sustain production. The certificate of a pilot who takes the Multi- Engine Land practical test in a Skymaster will be endorsed “For Centerline Thrust Only.” The newly minted twin pilot will have to be trained in and take another checkride in an airplane with wing-mounted engines to have this restriction removed. From the pilot’s perspective, a Skymaster with both engines running flies like a very capable single-engine airplane. Performance suffers drastically when either engine fails, of course, but the airplane climbs better with only the rear engine running than it does on the front engine alone. This is because the discharge airflow from the front engine is energized as it passes through the rotating rear propeller and hugs the fuse- lage. With the rear engine feathered, discharge air from the front propeller detaches from the fuselage, creating drag and reducing climb performance. Unlike most other twins, retracting the landing gear is not an immediate-action checklist item when an engine fails. Putting the gear switch in the “retract” position causes the gear doors (which are closed when the gear is down) to open while the gear is in transit, exposing large drag-producing openings. Skymaster pilots start the rear engine first, and let its instrument indications stabilize before starting the front engine. If the rear engine should shut down after the front engine is started, the pilot has nothing but instrument indications to rely on as a warning; there have been incidents/accidents when the pilot took off on the front engine only, unaware that the rear engine had failed. SAMPLE Chapter 1 The Concept of Multi-Engine Flying 7 1. What distinguishes a “light” twin from a “heavy” twin? A—A light twin weighs less than 6,000 pounds. B—A light twin’s VSO is less than 61 knots. C—Both A and B. 2. On a conventional twin, when an engine fails the airplane yaws toward A—the good engine. B—the critical engine. C—the failed engine. 3. If an airplane weighs less than 6,000 pounds and has a VSO of less than 60 knots, the manufac- turer must demonstrate that the airplane is able to climb at least _____ feet per minute on a stan- dard day at sea level with one propeller feathered. A—50 B—100 C—There is no minimum climb requirement. 4. If an airplane cannot climb with one propeller feathered, the reason is that A—drag is greater than lift. B—drag is greater than thrust. C—lift is greater than thrust. 5. Which statement concerning drag is true? A—Parasitic drag is greatest at low speed. B—Parasitic drag increases as speed increases. C—The airplane is most efficient when parasitic and induced drag are equal. 6. In a high-power, low-speed situation such as ini- tial climb, a propeller’s descending blade A—creates more torque than the ascending blade. B—creates more thrust than the ascending blade. C—is further from the centerline than the ascending blade. 7. The propeller of a failed engine creates the least drag when it is A—feathered. B—windmilling. C—stopped. 8. On an airplane with counter-rotating propellers, the _______ engine is the critical engine. A—right B—left C—Neither; there is no critical engine. 9. How can a pilot whose multi-engine rating is lim- ited to centerline thrust act as pilot-in-command of an airplane with wing-mounted engines? 10. When an engine fails on a twin-engine airplane, how much climb performance is lost? A—80 percent B—50 percent C—20 percent CHAPTER 1 Review Questions SAMPLE THE COMPLETE MULTI-ENGINE PILOT Pilots learning multi-engine flying have relied on this essential book for more than 20 years. Learn fundamentals of flying multi-engine airplanes and the aerodynamic laws that govern multi-engine flight under Bob Gardner’s experienced and energetic tutoring. This fifth edition includes a new chapter on energy management and information on both obtaining the multi-engine rating and checking out in a new twin. An integrated flight and ground syllabus details the program for the rating and provides a sample written test, typical of the one used for new-aircraft checkouts. Also contains a complete library of FAA source material on multi-engine flight subjects. The Complete Pilot series is designed for use in flight schools, for home study, and as a base for student kits. FIFTH EDITION Bob Gardner Aviation Supplies & Academics, Inc. 7005 132nd Place SE Newcastle, Washington 98059 USA 425-235-1500 | asa2fly.com ASA-MPT-5 TM Also in The Complete Pilot Series: The Complete Private Pilot The Complete Private Pilot Syllabus The Complete Advanced Pilot The Complete Remote Pilot From the Foreword by Barry Schiff: “By studying the principles Bob Gardner so eloquently discusses— and simplifies!—the challenging task of becoming a proficient and knowledgeable multi-engine pilot will become easier and more understandable.” ISBN 978-1-64425-195-9 TRANSPORTATION USD $24.95