48 Worked Examples: Anatomy, Regulations & Structures

The category of aircraft is “Airplane,” and its class is “Single Engine Land (SEL).”

1. Wings. H & O. The wings provide the primary lift force on the airplane to sustain its flight.
2. Vertical stabilizer. B. The vertical stabilizer gives the aircraft directional (yaw) stability.
3. Fuselage. A. The fuselage is the main body of the aircraft and houses the cockpit, engine, fuel, and various flight systems.
4. Flaps. F & P. The flaps allow the wings to sustain lift at low airspeeds and are used during takeoff and landing.
5. Undercarriage. I & K. The undercarriage is the wheels used to maneuver the aircraft on the ground.
6. Propeller. L. The propeller provides the propulsive force to move the airplane forward; it is connected to the engine.
7. Rudder. C. The rudder is used for directional (yaw) control.
8. Ailerons. G & P. The ailerons are differential flaps and are used for roll control.
9. Elevator. D. The elevator is used for pitch control.
10. Horizontal stabilizer. E. The horizontal stabilizer gives the aircraft stability in the pitch direction.
11. Wing strut. N. The purpose of the wing struts (one for each wing) is to carry tensile loads to resist wing bending from the lift forces.
12. Engine. M. The engine provides the power to spin the propeller and create thrust to propel the aircraft forward.

1. Main spar. A. The main spar will carry the primary bending loads on the wing. The main spar is usually a form of I-beam, which is strong, stiff, and light.
2. Main spar attachments. E. The main spar is attached to the fuselage using lugs and through bolts. The purpose of the spar attachments is to carry the bending loads through the fuselage from one wing to the other.
3. Root rib. D. The root rib is the strongest rib because it carries most of the torsion loads from the wing and transfers them to the fuselage structure.
4. Tip rib. I. The tip rib is the last and outermost rib in the wing structure, which because of the low loads there, can usually be made of the thinnest sheet material.
5. Rear spar. F. The rear spar carries some bending loads and attaches to the fuselage to carry torsion loads. The rear spar is also used to attach the flaps and the ailerons.
6. Ribs. B. The ribs define the wing’s cross-sectional (airfoil) shape and carry torsional loads. The ribs usually have lightening holes in their webs to reduce weight.
7. Stringers. C. The stringers increase the wing bending stiffness to help distribute the loads and prevent skin buckling.
8. Flap. G. The flaps are high-lift devices and allow the aircraft to fly at lower airspeeds for takeoff and landing.
9. Flap rib. H. The flap rib helps define the flap’s shape and carries torsional loads.

The International Civil Aviation Organization, or ICAO, is an agency of the United Nations founded in 1947. The ICAO is essential in civil aviation “To ensure international aviation is conducted in a unified, safe, and orderly manner.” They set standards and policies regarding international air transport based on “equality of opportunity, and so it is operated soundly and economically for the benefit of all.” The ICAO works with the member states and various aviation organizations at all levels to develop International Standards and Recommended Practices (SARPs), which form the basis for all civil aviation regulations worldwide, such as FAA FARs in the US and the EASA standards in Europe. The ICAO does not deal with military aviation, although military aircraft design standards are usually developed from the ICAO SARPs.

In 2013, the ICAO set a new noise standard, known as Chapter 14 or Stage 5, by the FAA. The new noise standard rules must be met by larger civil aircraft designed and certified for airworthiness after 2017 or smaller aircraft after 2020. The purpose of the new standard is to reduce the noise level for people frequently exposed to aircraft noise, including passengers, flight crews, and the people on the ground, particularly those who live in residential communities surrounding airports.

According to the ICAO, aircraft noise is considered the most significant cause of adverse community reactions related to the operation and expansion of airports. This issue persists even though the Stage 4 standard, adopted in 2006, has already reduced the Effective Perceived Noise Level (EPNdB) from the previous noise standards. The new Stage 5 standard requires a cumulative reduction of 7 EPNdB relative to the Stage 4 standard.

The first aircraft to be certified under the new noise standard was the De Havilland Canada Dash 8-400 turboprop aircraft, which underwent recertification tests to meet the latest noise standards of Chapter 14. The Dash 8-400 aircraft is the first turboprop aircraft to achieve this certification. According to EASA, about one-third of newer aircraft currently flying have already met the Stage 5 noise standard requirements. However, all new aircraft produced after 2020 will be held to these higher noise standards.

You can read about the role of the FAA in commercial space activities here: https://www.faa.gov/space/. The Office of Commercial Space Transportation (FAA/AST) regulates and oversees commercial space launches in the United States. The FAA/AST’s mission is to ensure the safety of the public, property, and the national security and foreign policy interests of the United States during commercial launches or reentry activities. The FAA/AST’s regulatory authority over commercial space transportation is limited to ensuring compliance with international obligations of the United States and protecting public health and safety, the safety of property, and national security and foreign policy interests of the United States.

The FAA/AST also aims to encourage, facilitate, and promote commercial space launches by the private sector, recommend appropriate changes in federal statutes, treaties, regulations, policies, plans, and procedures, and facilitate the strengthening and expansion of the United States space transportation infrastructure.

Any short discussion on any topic from PART 23 and PART 25 is acceptable. PART 23 considers AIRWORTHINESS STANDARDS: NORMAL CATEGORY AIRPLANES. The contents include standards for flight performance, flight characteristics, controllability, structural design, fire protection, etc. For example, under “Performance” we have:

23.2100 Weight and center of gravity.
23.2105 Performance data.
23.2110 Stall speed.
23.2115 Takeoff performance.
23.2120 Climb requirements.
23.2125 Climb information.
23.2130 Landing.

Using “Takeoff performance” as a further example, then we find a discussion on the following: Stall speed safety margins; Minimum control speeds, and climb gradients. For single engine airplanes and certain low-speed multi-engine airplanes, takeoff performance includes the determination of the ground roll and initial climb distance to 50 feet (15 meters) above the takeoff surface. For certain multi-engine airplanes, takeoff performance includes a determination of the following distances after a sudden critical loss of thrust, e.g., an aborted takeoff at critical speed, ground roll and initial climb to 35 feet (11 meters) above the takeoff surface, and takeoff flight path.

PART 25 considers AIRWORTHINESS STANDARDS: TRANSPORT CATEGORY AIRPLANES. Like Part 23 the contents include standards for flight performance, flight characteristics, controllability, structural design, powerplants, operating limitations, etc. For example, under “Operating Limitations” we have (in part):

25.1503 Airspeed limitations: general.
25.1505 Maximum operating limit speed.
25.1507 Maneuvering speed.
25.1511 Flap extended speed.
25.1513 Minimum control speed.
25.1515 Landing gear speeds.

Using “Landing gear speeds” as a further example, then we find a discussion of the established landing gear operating speed or speeds, VLO, which they say may not exceed the speed at which it is safe both to extend and to retract the landing gear, as determined under Part 25.729 or by flight characteristics. They go on further to say that for the aircraft if the extension speed is not the same as the retraction speed (meaning that the maximum safe retraction of the landing gear may not occur at the same airspeed as for the extension of the gear), the two speeds must be designated as VLO_EXT and VLO_RET, respectively. Finally, they conclude by saying that the established landing gear extended speed VLE may not exceed the speed at which it is safe to fly with the landing gear secured in the fully extended position.

The Federal Aviation Administration (FAA) has established the Federal Aviation Regulations (FARs) to regulate the use of drones, also known as Unmanned Aircraft Systems (UAS), in the National Airspace System (NAS). Part 107 of the FARs pertains specifically to small UAS operations, which includes commercial and non-recreational use of drones weighing less than 55 lb (24.9 kg). These regulations were introduced recently by the FAA because of the proliferation of various types of commercially available drones, some of which were being flown high and fast enough to pose a danger to other aviation operations or to the general public.

While the Part 107 rules are flexible to accommodate future technological innovations, they also impose restrictions on the flight operations of all types of drones for safety considerations. FAR Part 107 sets down a series of “common sense” rules requiring the drone operator to avoid all types of crewed aircraft and never operate such a drone carelessly or recklessly.

The specific reasons for FAA’s concerns regarding the continued introduction of diverse types of drones into the aviation spectrum include:

1. Safety: The primary concern of the FAA is the safety of people and property on the ground, as well as other aircraft in the air. Drones can collide with other aircraft or cause injury or damage.
2. Privacy: The use of drones has raised privacy concerns, as they can easily fly over private property and capture images and videos. The FAA must balance the privacy rights of individuals with the benefits of drone technology.
3. Security: Drones can be used for malicious purposes, such as smuggling, spying, and conducting attacks. The FAA must consider the security implications of drone operations and take measures to prevent unauthorized use.
4. Integration: The integration of drones into the NAS is a complex process, and the FAA must ensure that they do not interfere with other aircraft operations or cause air traffic control problems.

The concern of operating drones in the vicinity of the ERAU campus would be similar to the concerns the FAA has on a larger scale. The safety and security of students, faculty, and staff, would be the top priority, as well as avoiding potential interference with aircraft operations at the airport.

1. This image shows a monocoque or shell type of structure. A monocoque structure is a design in which the outer skin or shell provides most of the structural strength and stiffness without needing internal framing or bracing. In a monocoque structure, loads are all distributed through the skin, and the skin is usually made of a material that is strong and thick enough to carry the required loads. This approach can result in a lighter and more streamlined structure because it eliminates the need for any internal structure or fasteners such as rivets.
2. Monocoque structures are designed to be lightweight and strong, but they can be vulnerable to buckling. Buckling can occur when compressive forces cause the skin to deform (inward or outward), causing the shell structure to wrinkle and lose its rigidity and strength.
3. Buckling usually happens when a monocoque structure is subjected to excessive compressive, torsion, or bending loads. The primary consideration is usually any part of the structure under compressive loads.
4. To prevent buckling in a monocoque structure, various techniques can be used, such as adding stiffeners, ribs, or stringers to the internal structure. Increasing the thickness of the skin or changing its material are other options.
5. A monocoque structure is commonly used in aircraft and spacecraft where weight is critical. On an aircraft, monocoque structures can be found in fuselages and on lightly loaded parts such as control surfaces and trim tabs. On spacecraft, the crew module or capsule is usually a monocoque structure and may be made of sandwich construction. The payload fairing on a rocket is usually designed as a monocoque structure, with the skin and internal structure providing the required strength and stiffness.