Lesson Overview

The student should exhibit knowledge of the elements regarding airworthiness requirements as necessary based on their respective ACS/PTS.

References : 14 CFR Part 91

Elements
  1. FAR 91.3 - Responsibility and Authority of the PIC

  2. FAR 91.7 - Civil Aircraft Airworthiness

  3. FAR 91.9 - Civil Aircraft Flight Manual, Marking, and Placard Requirements

  4. FAR 91.203 - Civil Aircraft: Certifications Required

  5. FAR 91.205 - Instrument and Equipment Requirements

  6. FAR 91.213(d) - Inoperative Instruments and Equipment

  7. FAR 91.400’s - Maintenance, Preventative Maintenance, and Alterations (Subpart E)

  8. FAR 91.207 - Emergency Locator Transmitters (ELT)

Schedule
  1. Determining Weight and Balance

  2. Atmospheric Conditions and Performance

  3. Performance Charts

  4. Determining the Required Performance is Attainable

  5. Exceeding Airplane Limitations

Equipment
  1. White board and markers

  2. References

IP Actions
  1. Discuss lesson objectives

  2. Present Lecture

  3. Ask and Answer Questions

  4. Assign homework

SP Actions
  1. Participate in discussion

  2. Take notes

  3. Ask and respond to questions

Completion Standards

The lesson is complete when the student can explain, and when necessary locate, the elements and documents related to airworthiness requirements.

Instructor Notes

Attention

Just as you would never scuba dive without your regulator operating properly or sky dive without the rip cord functioning, you should never fly an airplane without essential equipment working properly. Unlike in a car, we do not have the option to pull over to the side of the road in the case of a problem.

Overview

Review Objectives and Elements/Key ideas

What

Airworthiness requirements are the basis for deciding whether an aircraft is worthy of safe flight. They are requirements that must be met to ensure an aircraft is safe and legal to fly.

Why

In order for an airplane to be airworthy certain documents must be on board and current, certain inspections must be completed, and certain instruments must be functioning, otherwise the airplane is unfit for flight and therefore un-airworthy or illegal to fly. An un-airworthy aircraft cannot be flown. Determining airworthiness can be very complex. This lesson is designed to provide a basis to make a decision regarding whether or not the airplane is airworthy.

Lesson Details

FAR 91.3 - Responsibility and Authority of the PIC

(a) The pilot in command of an aircraft is directly responsible for, and is the final authority as to, the operation of that aircraft.
(b) In an in-flight emergency requiring immediate action, the pilot in command may deviate from any rule of this part to the extent required to meet that emergency.
(c) Each pilot in command who deviates from a rule under paragraph (b) of this section shall, upon the request of the Administrator, send a written report of that deviation to the Administrator.

FAR 91.7 - Civil Aircraft Airworthiness

(a) No person may operate a civil aircraft unless it is in an airworthy condition.
(b) The pilot in command of a civil aircraft is responsible for determining whether that aircraft is in condition for safe flight. The pilot in command shall discontinue the flight when unairworthy mechanical, electrical, or structural conditions occur.

For the best definition of airworthiness, read the Airworthiness Certificate. The Authority and Basis for Issuance states the aircraft must conform to the type certificate. The aircraft cannot be changed from its type certificate; must be in the condition in which it left the factory. The only way the airplane can be changed is with a supplemental type certificate. The Terms and Conditions states that the aircraft must be maintained in accordance with the FARS. The PIC of a civil aircraft is responsible for determining whether that aircraft is in condition for safe flight and shall discontinue the flight when un-airworthy mechanical, electrical, or structural conditions occur. This is the only FAR which mentions a visual inspection (i.e. condition for safe flight).

FAR 91.9 - Civil Aircraft Flight Manual, Marking, and Placard Requirements

(a) Except as provided in paragraph (d) of this section, no person may operate a civil aircraft without complying with the operating limitations specified in the approved Airplane or Rotorcraft Flight Manual, markings, and placards, or as otherwise prescribed by the certificating authority of the country of registry.
(b) No person may operate a U.S.-registered civil aircraft—
  (1) For which an Airplane or Rotorcraft Flight Manual is required by §21.5 of this chapter unless there is available in the aircraft a current, approved Airplane or Rotorcraft Flight Manual or the manual provided for in §121.141(b); and
  (2) For which an Airplane or Rotorcraft Flight Manual is not required by §21.5 of this chapter, unless there is available in the aircraft a current approved Airplane or Rotorcraft Flight Manual, approved manual material, markings, and placards, or any combination thereof.
(c) No person may operate a U.S.-registered civil aircraft unless that aircraft is identified in accordance with part 45 of this chapter.
(d) Any person taking off or landing a helicopter certificated under part 29 of this chapter at a heliport constructed over water may make such momentary flight as is necessary for takeoff or landing through the prohibited range of the limiting height-speed envelope established for the helicopter if that flight through the prohibited range takes place over water on which a safe ditching can be accomplished and if the helicopter is amphibious or is equipped with floats or other emergency flotation gear adequate to accomplish a safe emergency ditching on open water.

FAR 91.203 - Civil Aircraft: Certifications Required

(a) Except as provided in §91.715, no person may operate a civil aircraft unless it has within it the following:
  (1) An appropriate and current airworthiness certificate. Each U.S. airworthiness certificate used to comply with this subparagraph (except a special flight permit, a copy of the applicable operations specifications issued under §21.197(c) of this chapter, appropriate sections of the air carrier manual required by parts 121 and 135 of this chapter containing that portion of the operations specifications issued under §21.197(c), or an authorization under §91.611) must have on it the registration number assigned to the aircraft under part 47 of this chapter. However, the airworthiness certificate need not have on it an assigned special identification number before 10 days after that number is first affixed to the aircraft. A revised airworthiness certificate having on it an assigned special identification number, that has been affixed to an aircraft, may only be obtained upon application to the responsible Flight Standards office.
  (2) An effective U.S. registration certificate issued to its owner or, for operation within the United States, the second copy of the Aircraft registration Application as provided for in §47.31(c), a Certificate of Aircraft registration as provided in part 48, or a registration certification issued under the laws of a foreign country.
(b) No person may operate a civil aircraft unless the airworthiness certificate required by paragraph (a) of this section or a special flight authorization issued under §91.715 is displayed at the cabin or cockpit entrance so that it is legible to passengers or crew.
(c) No person may operate an aircraft with a fuel tank installed within the passenger compartment or a baggage compartment unless the installation was accomplished pursuant to part 43 of this chapter, and a copy of FAA Form 337 authorizing that installation is on board the aircraft.
(d) No person may operate a civil airplane (domestic or foreign) into or out of an airport in the United States unless it complies with the fuel venting and exhaust emissions requirements of part 34 of this chapter.

The airworthiness certificate must be displayed in the cabin or cockpit entrance so that it is legible to passengers or crew.

FAR 91.205 - Instrument and Equipment Requirements

This FAR details the bare minimum instruments and equipment required for day/night VFR flight and IFR flight. Two nmenomics that can assist with remembering the lengthy list of required equipment are :

VFR - A TOMATO FLAMES (day) and FLAPS (night)
  • A – Altimeter

  • T – Tachometer

  • O – Oil Temperature Gauge

  • M – Manifold Pressure Gauge (If applicable)

  • A – Airspeed Indicator

  • T – Temperature Gauge (For each liquid cooled engine)

  • O – Oil Pressure Gauge

  • F – Fuel Gauges

  • L – Landing Gear Position Indicator (If applicable)

  • A – Anti Collision Lights (For aircraft manufactured after March 11, 1996)

  • M – Magnetic Compass

  • E – ELT

  • S – Seat Belts

And for night flight add :

  • F – Fuses

  • L – Landing Light

  • A – Anti Collision Lights

  • P – Position Lights

  • S – Source of Power

IFR - GRABCARD
  • G -Generator or Alternator

  • R - Radio/Navigation Appropriate For Flight

  • A - Attitude Indicator

  • B - Ball (Inclinometer)

  • C - Clock

  • A - Altimeter (Pressure Sensitive)

  • R - Rate of Turn Indicator

  • D - Directional Gyro

FAR 91.213(d) - Inoperative Instruments and Equipment

  1. MEL

    1. An FAA approved listing of instruments/equipment that may be inoperable and remain airworthy

  2. Without an MEL - 91.213(d)

    1. Follow the flow provided in AC 91-67

      1. Is it required by the aircrafts equipment list or the kinds of equipment list?

      2. Is it required by the VFR type certificate requirements prescribed in the airworthiness certification requirements?

      3. Is it required by an AD?

      4. Is it required by FAR 91.205, 91.207, etc.?

      5. If no, the inoperative equipment must be removed or deactivated and placarded as inoperative

        1. 91.405 - Inoperative equipment must be repaired, replaced, removed at the next required inspection

        2. Finally, the PIC decides whether the equipment creates a hazard for the anticipated flight

FAR 91.400’s - Maintenance, Preventative Maintenance, and Alterations (Subpart E)

  1. FAR 91.401 - Applicability

    1. Rules governing maintenance, preventative maintenance, alterations of US registered civil aircraft

  2. FAR 91.405 - Maintenance Required

    1. Each owner or operator of an aircraft:

      1. Shall have that aircraft inspected as prescribed in subpart E of this part and shall between required inspections, have discrepancies repaired as prescribed in part 43 of this chapter

      2. Shall ensure that maintenance personnel make appropriate entries in the aircraft maintenance records indicating the aircraft has been approved for return to service

      3. Shall have any inoperative instrument/equipment, permitted to be inoperative by §91.213(d)(2) of this part, repaired, replaced, removed, or inspected at the next required inspection

      4. When listed discrepancies include inoperative instruments or equipment, shall ensure that a placard has been installed as required by §43.11 of this chapter.

  3. FAR 91.409 - Inspections

    1. Annual Inspection requirement

      1. 100 hour inspection requirement, if for rent or for hire

  4. FAR 91.411 - Altimeter system and Altitude Reporting Equipment Tests and Inspections

    1. Static Pressure System and Altimeter tests required for IFR flight

      1. Required every 24 calendar months

  5. FAR 91.413 - ATC Transponder Tests and Inspections

    1. Transponder tests and inspections required

      1. Required every 24 calendar months

FAR 91.207 - Emergency Locator Transmitters (ELT)

  1. Inspection requirements

    1. Every 12 calendar months

  2. The batteries must be replaced (or recharged)

    1. When the transmitter has been in use more than 1 cumulative hour

    2. When 50% of their useful life has expired

Conclusion

Through the FARS mentioned here, we find that the PIC is the final authority as to the safety of the flight. Airworthiness requires conforming to the type certificate, as well as the required maintenance and inspections. To be airworthy, the documents required onboard are the airworthiness certificate, the registration, operating limitations (AFM), as well as the weight and balance (part of the type certificate). We have found the required equipment as well as the process for determining whether the airplane is airworthy in the case of inoperative equipment. Finally, the FARs provided the necessary inspections needed to maintain airworthiness.

ACS Requirements

To determine that the applicant exhibits instructional knowledge of the elements related to required airworthiness by describing:

  1. Required instruments and equipment for day/night VFR.

  2. Procedures and limitations for determining airworthiness of the airplane with inoperative instruments and equipment with and without a minimum equipment list (MEL).

  3. Requirements and procedures for obtaining a special flight permit.

  4. Airworthiness directives, compliance records, maintenance/inspection requirements, and appropriate records.

  5. Procedures for deferring maintenance on aircraft without an approved MEL.