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Interagency Aviation Accident Prevention Bulletin 26-06: Aircraft Engine Carburetor Heat Rigging

· DOI Office of Aviation Services · 2026

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Overview

The Interagency Aviation Accident Prevention Bulletin 26-06: Aircraft Engine Carburetor Heat Rigging () is a public-domain DOI Office of Aviation Services aviation safety document, republished here as a free chaptered HTML edition with a linked table of contents and the official PDF.

Publisher
DOI Office of Aviation Services
Document
Year
2026
Pages
2

Key points

  • Improperly rigged carburetor heat systems can lead to carburetor icing, partial power loss, or complete engine failure.
  • Pilots should ensure carburetor heat controls move smoothly and verify positive detents at both ends of travel during preflight inspections.
  • Carburetor icing can occur at temperatures as high as 90°F and relative humidity levels as low as 35 percent.
  • Full carburetor heat should always be applied to prevent icing; partial application may increase the risk of icing.
  • Thorough functional checks of the carburetor heat system are essential, especially after maintenance, to confirm proper operation.
Frequently asked questions
What should pilots check during preflight inspections regarding carburetor heat?

Pilots should ensure the carburetor heat control moves smoothly throughout its full range of travel and verify positive detents at both ends of travel.

What are the conditions under which carburetor icing can occur?

Carburetor icing can occur at temperatures as high as 90°F and relative humidity levels as low as 35 percent.

What is the recommended action if unexpected RPM or manifold pressure drops occur?

If RPM or manifold pressure drops unexpectedly, or if engine roughness develops, pilots should immediately apply full carburetor heat.

Why is it important to conduct functional checks of the carburetor heat system?

Functional checks are essential to confirm proper operation and prevent avoidable power loss or engine failure, especially after maintenance.

What is the minimum acceptable RPM drop during engine run-up when applying carburetor heat?

While the AFM/POH specifies a minimum of 75 RPM drop, operational experience may suggest higher expectations, such as at least 100 RPM for the DOI fleet.

Document

OAS-43A (12/12)

Interagency Aviation

Accident Prevention Bulletin

No. IA APB 26-06 June 2 5 , 2026 Page 1 of 2 Subject: Aircraft Engine Carburetor Heat Rigging Area of Concern: Preflight Inspection/Flight Safety Distribution: All Aviation Operations Discussion: This Accident Prevention Bulletin highlights a recurring hazard involving improperly rigged or partially functional carburetor heat systems identified during interagency operations and supported by general aviation accident data. Reduced carburetor heat effectiveness can result in undetected carburetor icing, partial power loss, or complete engine failure.

In carbureted piston engine airplanes, air passing through the carburetor can cool rapidly and form ice which will restrict air and fuel flow reducing engine power even in mild temperatures. Carburetor heat is a control in many piston aircraft that directs warm air into the carburetor to prevent or remove carburetor ice. Pilots typically use it during low power settings (like descent) or anytime carb ice is suspected.

During a recent post-maintenance preflight inspection following engine removal/replacement and an annual inspection, a DOI pilot identified an improperly rigged carburetor heat system on a CC18-180 Top Cub. The carburetor heat control exhibited abnormal stiffness and lacked the expected positive detents (“clicks”) at the limits of travel. During engine run-up, the RPM drop observed during carburetor heat application ranged from only 25–150 RPM, compared to the DOI fleet expectation of at least 100 RPM and 175 for Top Cubs. Although the Top Cub combined Aircraft Flight Manual/Pilot Operating Handbook (AFM/POH) specified only a minimum 75 RPM drop, further inspection revealed the carburetor heat door was not fully opening or closing due to improper rigging. Had the pilot relied solely on the checklist procedures contained in the AFM/POH, the deficiency may not have been detected.

A previous DOI fleet mission experienced an in-flight engine failure resulting in a forced landing due to inadequate carburetor heat rigging. Additional events have involved kinked, binding, or broken carburetor heat cables that degraded system performance.

The National Transportation Safety Board (NTSB) has investigated multiple accidents involving ineffective or improperly functioning carburetor heat systems, including a recent accident in Alaska, ANC25LA025 - Investigation .

Recommended Preflight and Operational Best Practices Pilots should follow AFM/POH procedures for verifying carburetor heat operation before flight; however, additional functional checks may be necessary to ensure proper system performance.

No. IA APB 26-06 June 24, 2026 Page 2 of 2 • During cockpit preflight inspection, ensure the carburetor heat control moves smoothly throughout its full range of travel, rather than verifying only the “OFF/COLD” position.

• Verify positive detents (“clicks”) at both ends of travel, indicating fully open and closed positions. Conduct a visual inspection if necessary.

• During engine run-up, confirm the RPM drop is appropriate for the aircraft and engine installation. While the AFM/POH provides minimum acceptable values, operational experience with specific aircraft may provide additional insight into normal system performance.

• When system functionality is in question, consult qualified maintenance personnel before flight.

Carburetor Heat Use Carburetor icing can occur at temperatures as high as 90°F and relative humidity levels as low as 35 percent. Pilots should reference the FAA’s Special Airworthiness Information Bulletin, SAIB-CE-09- 35 for safety guidance and the Carburetor Icing Probability Chart to evaluate potential icing conditions.

Best Practices for Carburetor Heat Use: • Use carburetor heat proactively to prevent ice formation, particularly prior to descents and during low-power operations.

• Apply carburetor heat before approach and descent whenever operating at low power settings or when atmospheric conditions are conducive to carburetor icing.

• Always apply full carburetor heat. Partial application may increase the likelihood of icing.

• If RPM or manifold pressure drops unexpectedly, or if engine roughness develops, immediately apply full carburetor heat.

Key Takeaway Carburetor icing can gradually rob an engine of power, often with little warning. A moving carburetor heat control doesn’t guarantee the system is working properly. Thorough functional checks—especially after maintenance—are essential to confirm proper operation and prevent avoidable power loss or engine failure.

/s / Keith C. Raley /s/ Lori Clark Keith C. Raley Lori Clark Division Chief, Aviation Safety and Training Branch Chief - Aviation Safety Aviation Operations and Management Management Systems U.S. Wildland Fire Service USDA, Forest Service U.S Department of the Interior

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Source: doi.gov. Public-domain U.S. Government work (17 USC §105) — freely reproducible.

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Document details

Doc number
Publisher
DOI Office of Aviation Services
Year
2026
Pages
2
File size
311 KB