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  4. Part 25
  5. § 25.1321
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14 CFR · Part 25

14 CFR § 25.1321

Arrangement and visibility.

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Read in Subpart F
Part 25 Contents
  • Special Federal Aviation Regulation No. 13
  • Special Federal Aviation Regulation No. 109
  • Subpart A: General
  • Subpart B: Flight
  • Subpart C: Structure
  • Subpart D: Design and Construction
  • Subpart E: Powerplant
  • Subpart F: Equipment
  • Subpart G: Operating Limitations and Information
  • Subpart H: Electrical Wiring Interconnection Systems (EWIS)
  • Subpart I: Special Federal Aviation Regulations
  • Appendix A to Part 25
  • Appendix B to Part 25
  • Appendix C to Part 25
  • Appendix D to Part 25
  • Appendix E to Part 25
  • Appendix F to Part 25
  • Appendix H to Part 25: Instructions for Continued Airworthiness
  • Appendix I to Part 25: Installation of an Automatic Takeoff Thrust Control System (ATTCS)
  • Appendix J to Part 25: Emergency Evacuation
  • Appendix K to Part 25: Extended Operations (ETOPS)
  • Appendix L to Part 25: HIRF Environments and Equipment HIRF Test Levels
  • Appendix M to Part 25: Fuel Tank System Flammability Reduction Means
  • Appendix N to Part 25: Fuel Tank Flammability Exposure and Reliability Analysis
  • Appendix O to Part 25: Supercooled Large Drop Icing Conditions
(a)

Each flight, navigation, and powerplant instrument for use by any pilot must be plainly visible to him from his station with the minimum practicable deviation from his normal position and line of vision when he is looking forward along the flight path.

(b)

The flight instruments required by § 25.1303 must be grouped on the instrument panel and centered as nearly as practicable about the vertical plane of the pilot's forward vision. In addition—

(1)

The instrument that most effectively indicates attitude must be on the panel in the top center position;

(2)

The instrument that most effectively indicates airspeed must be adjacent to and directly to the left of the instrument in the top center position:

(3)

The instrument that most effectively indicates altitude must be adjacent to and directly to the right of the instrument in the top center position; and

(4)

The instrument that most effectively indicates direction of flight must be adjacent to and directly below the instrument in the top center position.

(c)

Required powerplant instruments must be closely grouped on the instrument panel. In addition—

(1)

The location of identical powerplant instruments for the engines must prevent confusion as to which engine each instrument relates; and

(2)

Powerplant instruments vital to the safe operation of the airplane must be plainly visible to the appropriate crewmembers.

(d)

Instrument panel vibration may not damage or impair the accuracy of any instrument.

(e)

If a visual indicator is provided to indicate malfunction of an instrument, it must be effective under all probable cockpit lighting conditions.

Regulations Referenced

14 CFR 25.1303

Reflects the eCFR edition current as of September 29, 2026. Retrieved from ecfr.gov on October 16, 2026.

Primary Source

  • Official Source (14 CFR · Part 25)