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Attitude Instrument FlyingInstrument Rating

Partial Panel Flying: Techniques Without Gyroscopic Instruments

Partial panel flying requires controlling the aircraft using only non-gyroscopic instruments when attitude indicator or heading indicator fail, demanding disciplined cross-check of remaining gauges to maintain safe flight.

Reviewed & updated · Grounded in current FAA handbooks & the ACS

Imagine cruising in IMC when your vacuum pump fails silently. The attitude indicator begins to slowly tumble, the heading indicator drifts to a stop, and suddenly the two instruments you rely on most for spatial orientation are gone. This is not a hypothetical scenario — vacuum system failures occur in general aviation, and when they do, a pilot who has not practiced partial panel flying is in serious danger. Partial panel flying is the discipline of controlling the aircraft for attitude, heading, altitude, and airspeed using only the instruments that remain functional — primarily the pitot-static instruments and the magnetic compass — without the gyroscopic attitude indicator (AI) and heading indicator (HI).

Understanding and practicing partial panel techniques is a required skill for the instrument rating and, more importantly, a genuine life-safety competency. The FAA's Instrument Flying Handbook (FAA-H-8083-15) dedicates substantial coverage to this skill precisely because spatial disorientation kills quickly once a pilot loses reliable attitude reference. This article walks through the instruments available, the techniques for using them, and the practical discipline required to survive and navigate a partial panel scenario.

Which Instruments Remain Available

Most light general aviation aircraft use a vacuum system to drive the attitude indicator and the heading indicator. Both instruments become unreliable following a vacuum failure. What remains are the pitot-static instruments — the airspeed indicator (ASI), altimeter, and vertical speed indicator (VSI) — and the turn coordinator (which is typically electrically driven and therefore survives a vacuum failure), plus the magnetic compass. Together, these four instrument types provide all the information needed to fly safely and navigate, but they demand a different scanning technique and a much higher mental workload.

It is worth noting that in some aircraft, both instruments may be electrically powered, or both vacuum-powered. Always know your specific aircraft's system architecture before flight. Regardless, partial panel technique assumes you have lost the AI and HI and must substitute the remaining instruments.

The Substitute Attitude Reference: Airspeed, Altimeter, VSI, and Turn Coordinator

Without the attitude indicator, you reconstruct pitch and bank attitude indirectly from the instruments that respond to it.

Controlling Pitch

Pitch attitude determines whether the aircraft is climbing, descending, or flying level. On partial panel, the airspeed indicator is your primary pitch reference for a given power setting. If you hold power constant, a nose-high attitude will cause airspeed to decrease and the VSI to show a climb; a nose-low attitude will cause airspeed to increase and the VSI to show a descent. The altimeter confirms whether altitude is being held. The VSI shows the trend and rate of altitude change, though it lags several seconds behind actual changes. Together, these three instruments give you a reliable, if slightly delayed, picture of pitch attitude. The key discipline is to make small, deliberate control inputs and then wait for the instruments to respond before making further corrections — chasing the VSI with large inputs typically causes pilot-induced oscillations.

Controlling Bank and Heading

The turn coordinator provides bank information via its miniature airplane symbol, which indicates the rate of turn. A standard-rate turn is indicated when the miniature airplane's wing aligns with the turn index marks; this corresponds to a turn rate of 3 degrees per second, completing a 360-degree turn in two minutes. When the wings are level on the turn coordinator, the aircraft is in coordinated wings-level flight — use this as your primary bank reference. The ball (inclinometer) in the turn coordinator indicates coordination; keep the ball centered with rudder pressure, as always.

Heading tracking is the most challenging aspect of partial panel. The magnetic compass becomes your only heading reference, but it has well-known errors that become critical in IMC:

  • Oscillation error: The compass swings and oscillates in turbulence, making it hard to read precisely.
  • Northerly turning error: In the northern hemisphere, when turning through north, the compass lags behind the actual heading. When turning through south, it leads. The memory aid is that the compass reads a heading opposite to the direction of turn when passing north, and in the direction of turn when passing south.
  • Acceleration/deceleration error: On easterly or westerly headings, accelerating causes the compass to indicate a turn toward north; decelerating causes it to indicate a turn toward south. This error is greatest on east and west headings and essentially absent on north and south headings.

Because of these errors, pilots use timed turns rather than watching the compass needle during the turn. At standard rate (3°/second), a 90-degree turn takes 30 seconds, a 180-degree turn takes 60 seconds, and a full 360-degree turn takes 120 seconds. Plan turns by calculating the time required and rolling out when that time has elapsed, then verify the approximate heading on the compass after the aircraft has stabilized. For compass turns, apply the standard corrections: when turning to a northerly heading in the northern hemisphere, roll out early by the amount of the compass lag (approximately equal to your latitude); when turning to a southerly heading, roll out late by a similar amount.

The Partial Panel Scan Pattern

Full-panel instrument flying uses the attitude indicator as the centerpiece of the scan, with supporting glances to the other instruments. Partial panel requires a fundamentally different scan because there is no single instrument that directly shows attitude. Instead, the pilot must cross-check all remaining instruments continuously and equally, building a composite picture of attitude from multiple indirect indicators.

A useful partial panel scan cycles through: turn coordinator (bank?) → airspeed indicator (pitch trend?) → altimeter (altitude holding?) → VSI (climb or descent rate?) → magnetic compass (heading approximate?) → back to turn coordinator. This cycle should be deliberate, methodical, and unhurried. One of the most dangerous partial panel habits is fixating on one instrument — particularly the airspeed indicator — while ignoring the others. Fixation is a well-documented contributor to loss of control.

Reducing workload is essential. As soon as you recognize a gyro failure, engage the autopilot if available — many autopilots operate on the turn coordinator's electrical gyro rather than the vacuum AI, and may continue to function normally. Declare an emergency if needed, advise ATC, and request vectors or a lower workload environment (e.g., a long final or a wider radar-vectored approach). The goal is to reduce the number of tasks competing for your limited attention.

Recognizing Gyroscopic Instrument Failure

Gyroscopic failures are insidious because they are rarely sudden. A failing vacuum pump causes instruments to slowly become unreliable, often with the AI tilting subtly and presenting false attitude information. The most dangerous scenario is the pilot who trusts a slowly failing AI over the pitot-static instruments, leading to controlled flight into terrain or spatial disorientation. Clues to a vacuum failure include: the AI showing a bank while the turn coordinator shows wings-level; the vacuum gauge (if installed) reading below the normal range of approximately 4.5 to 5.5 inches Hg; or the HI drifting more than the normal allowable amount (roughly 3 degrees per 15 minutes). If you suspect a gyro failure, cover the AI and HI immediately with the instrument covers provided in many cockpits, or at least mentally discount them and fly the partial panel instruments.

Key Numbers and Rules

  • Standard-rate turn: 3 degrees per second; 2 minutes for a full 360-degree turn.
  • Timed turns: 30 seconds for 90°, 60 seconds for 180°, 120 seconds for 360° at standard rate.
  • Normal vacuum system pressure: approximately 4.5 to 5.5 inches Hg in most light aircraft.
  • HI acceptable precession rate: no more than approximately 3 degrees per 15 minutes of flight.
  • Compass northerly turning error: compass lags through north, leads through south (in northern hemisphere).
  • Acceleration error: greatest on east and west headings; accelerating = apparent turn toward north.

Memory Aid

"UNOS" — a commonly taught compass turning memory aid: Undershoot North, Overshoot South. When rolling out to a northerly heading, stop the turn a few degrees early (undershoot) because the compass lags; when rolling out to a southerly heading, roll out a few degrees late (overshoot) because the compass leads. The number of degrees to undershoot or overshoot is approximately equal to your latitude.

Common Test Traps

  • Confusing which instruments fail with a vacuum failure: The turn coordinator is typically electrically driven and survives vacuum failure — do not mark it as failed. The AI and HI are vacuum-driven and fail. Know your aircraft's specific system.
  • Misidentifying the primary pitch instrument: On partial panel in straight-and-level flight, the altimeter is the primary pitch instrument (it directly shows whether altitude is maintained); airspeed is the supporting instrument. On full panel, the AI is primary — the distinction matters for exam questions.
  • Forgetting that compass errors are heading-dependent: Acceleration error is greatest on east and west; turning error is greatest near north and south. The FAA test will probe whether you know which error applies on which heading.
  • Assuming the turn coordinator shows bank angle: The turn coordinator shows rate of turn, not bank angle directly. A standard-rate turn in a light aircraft typically requires about 15–20 degrees of bank, but the instrument does not display a specific angle — it shows whether you are turning at standard rate or not.
  • Treating partial panel as a last resort only: Some students assume partial panel is only for emergencies. In fact, practicing partial panel regularly is required for instrument proficiency, and approaches must sometimes be flown partial panel for a checkride. Treat it as a normal skill, not an exotic emergency procedure.

Frequently asked questions

What instruments are available for partial panel flying when the gyroscopic instruments fail?

When the attitude indicator and heading indicator are inoperative, pilots rely on the non-gyroscopic instruments: the airspeed indicator, altimeter, vertical speed indicator, turn coordinator (which uses a gyro but is typically on a separate vacuum or electrical source), and magnetic compass. These instruments together provide enough pitch, bank, and directional information to maintain controlled flight. The Instrument Flying Handbook (IFH) emphasizes that a disciplined, systematic cross-check of these remaining gauges is essential to compensate for the loss of the primary attitude references.

How do you maintain heading during partial panel flight without a heading indicator?

Without a functioning heading indicator, pilots must rely on the magnetic compass for directional reference, which requires understanding its inherent errors including northerly turning error, acceleration error, and the compass's tendency to lag or lead during turns. A common technique is to use timed turns based on the turn coordinator's standard-rate indication (3 degrees per second) to roll out on a desired heading, accounting for compass error corrections. The IFH recommends that pilots practice these timed turn techniques regularly so they can execute them accurately under the stress of an actual partial panel situation.

Why is partial panel flying considered more demanding than full panel instrument flying?

Partial panel flying is more demanding because the pilot loses the two instruments—the attitude indicator and heading indicator—that provide the most immediate and intuitive picture of aircraft attitude and direction, forcing reliance on instruments that are slower to respond or inherently less precise. The increased workload requires a more deliberate and disciplined cross-check pattern, as described in the Instrument Flying Handbook, to derive pitch and bank information indirectly from the altimeter, airspeed indicator, and vertical speed indicator. Additionally, the magnetic compass introduces errors that must be mentally corrected in real time, adding cognitive load during an already high-stress emergency situation.

See also

FAA source

Instrument Flying Handbook (FAA-H-8083-15), Chapters 5 and 7; Pilot's Handbook of Aeronautical Knowledge (FAA-H-8083-25), Chapter 8

This page is an original, plain-English summary grounded in the public-domain FAA handbook cited above. Click the citation to open the official FAA handbook PDF. It is a study aid, not a substitute for the official handbook or the regulations.

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