Aircraft
Certification Service Washington, DC U.S. Department of Transportation Federal Aviation Administration
NE-10-05
October 16, 2009
This is information only. Recommendations
aren’t mandatory.
Introduction
This Special Airworthiness Information Bulletin (SAIB) alerts you,
pilots, owners, operators, maintenance personnel, and certificated
repair facilities of reciprocating aircraft engines with float-type
carburetors, of potential hazards associated with those carburetors. At
this time, the airworthiness concern is not an unsafe condition that
would warrant airworthiness directive (AD) action under Title 14 of the
Code of Federal Regulations (14 CFR) part 39.
Background
This SAIB results from reports of numerous accidents and incidents over
the past 20 years that resulted from an engine stoppage or engine fire
involving float-type carburetors. Numerous service information letters
(SILs) and service bulletins (SBs) were issued during that time to
address floattype carburetor issues related to poor idle cut-off and
fuel leaking from the carburetor after engine shutdown. The FAA issued
SAIB CE-06-33R1 in April 2006 to address those conditions. These
conditions are often the result of fuel leaking into the carburetor
float, a damaged or worn float, or a damaged or worn float valve.
Despite the availability of the SILs and SBs, the FAA is still
receiving reports of accidents and incidents resulting from carburetor
float anomalies. In comparison to the SILs and SBs previously issued,
this SAIB is applicable to all aircraft with reciprocating engines with
float-type carburetors installed and provides more detail and focused
recommended actions.
Carburetor float design has evolved over the past 20 years, resulting
in many different types of floats in service today. Carburetor floats
are primarily made from polymers (plastics), brass, or epoxy “foam”.
The buoyancy of a float is typically provided by either a cavity, or
cavities, that are formed by a thin outer shell of polymer, brass, or
epoxy. If this shell is compromised, the result is a breach that
permits fuel to enter the cavity, which reduces the buoyancy of the
float. The shell can be compromised in several ways such as:
Cracking
Separating at a weld seam, soldered seam, or joint
A hole.
A hole can be caused by the shell
rubbing on the carburetor bowl. The shell might rub on the carburetor
bowl due to excessive pivot wear, which affects the alignment and
operation of the float and metering components. If the float buoyancy
is reduced, it can lead to improper metering of fuel to the engine
and/or fuel leaking from the carburetor. These conditions can then lead
to complete loss of power or engine fires. Some newer float designs are
fabricated from closed cell epoxy material. These floats are more
tolerant to rubbing, chafing, and cutting since the buoyancy is
provided by thousands of independent closed cells rather than a few
closed cells.
Carburetors are commonly maintained only when problems warrant their
repair or overhaul. However, it is recommended by engine type
certificate holders that carburetors be overhauled at the engine's
overhaul interval. If this is not done, the airworthiness of the
carburetor can deteriorate and eventually cause a severe hazard to
operation.
Applicable model list: All aircraft with reciprocating engines with float-type carburetors installed.
Recommendations
Pilot Action:
During preflight
inspections, examine the engine area for evidence of fuel leakage.
During engine start, be alert for carburetor flooding or the need for
excessive leaning. Hard starting might be an indicator of a
deteriorating or damaged carburetor float. During engine operation,
excessive fuel consumption and/or poor idle performance might indicate
a deteriorating or damaged carburetor float. Difficulty shutting down
the engine with the mixture cut-off control might be an indicator of a
deteriorating or damaged carburetor float. If any of these conditions
are observed, the pilot should have qualified maintenance personnel
inspect the aircraft before the next flight.
Owner, Operator, and Maintenance Personnel Action:
Perform routine carburetor
inspections for signs of fuel leakage. Inspect for fuel stains from the
bowl vents in the throat of the carburetor and/or fuel in the air box.
Comply with all engine and carburetor manufacturer recommendations,
including, but not limited to, maintenance procedures, SBs, Customer
Bulletins, SILs, etc. Maintenance Personnel addressing these issues
should inspect the carburetor for signs of fuel leakage. Remove
carburetors with signs of fuel leakage and send them to a qualified
repair station for overhaul, inspection, and repair.
Overhaul Action:
Overhaul the carburetor at
every engine overhaul interval. The correct interval to use is
whichever of the following occurs first:
The engine manufacturer’s recommended interval
12 years
2,400 hours
During overhaul, inspect the float and float valve. Replace with a new float and float valve as necessary.
For Further Information Contact
Mr. Sanford Proveaux, Aerospace Engineer, Atlanta Aircraft
Certification Office, FAA, Small Airplane Directorate, Propulsion and
Services Branch, 1701 Columbia Avenue, College Park, GA 30337;
telephone (404) 474-5566; fax (404) 474-5606; e-mail:
sanford.proveaux@faa.gov.