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Aircraft Fuel System; water contamination of fuel tank systems on SAIB CE-10-40R1
Aircraft Fuel System; water contamination of fuel tank systems on SAIB CE-10-40R1
SPECIAL AIRWORTHINESS FAA
Aviation Safety INFORMATION BULLETIN
SUBJ: Aircraft Fuel System; water contamination of fuel tank systems on SAIB: CE-10-40R1
Cessna single engine airplanes Date: July 30, 2010
This is information only. Recommendations aren¡¦t mandatory.
Introduction
This Special Airworthiness Information Bulletin is to inform pilots, owners, operators, and maintenance
and service personnel of Cessna Aircraft Company (and formerly Reims Aviation S.A.) Model 100,
200, or 300 series, any model and/or prefix and/or suffix in the series of airplanes as applicable of
the hazards associated with water contamination of fuel tank systems. The fuel tank system consists of
all tanks, components, lines, fittings, etc., from the fuel tank to the engine.
This SAIB revises SAIB CE-10-40, dated July 27, 2010 as a result of comments received from an
organization and other airworthiness authorities. It adds to the list of models potentially affected.
At this time, the FAA has determined that this 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
Recent safety information on Cessna 150, 170, and 172 series airplanes caused us to re-examine our
efforts on preventing accidents and incidents due to water contaminated fuel. Water may enter the fuel
tank system via any penetration in the wing fuel tank. Water in the fuel may come out of solution, settle
and make its way to a drain location in the form of a blob, pea, or BB-shaped translucent mass found at
the bottom of the sampler cup. Water suspended in the fuel may lead to a cloudy or hazy appearance in
the sampler cup. Water may have dissolved in the fuel, but the conditions have not yet occurred to cause
the water to come out of solution and perhaps adhere to the dry tank upper surface or walls (similar to
condensation). Understanding this, all pilots, owners, operators, maintenance, and service personnel of
these type airplanes should assume some water exists in the fuel tank system on the airplane.
Recommendations
We recommend you do the following:
1. Check your fuel tank system to assure it is equipped with fuel drain valves (not plugs) at all
permissible drain locations (i.e.; wing tanks, manifold tanks, selector valves, shut-off valves, strainers,
low points, etc.). Become familiar with all drain locations on a specific model of airplane. From model
to model in a series of airplanes, the number, type, and location of drains may not be the same. There is
no single point of drainage that can be used to check for all fuel system contaminants simultaneously.
Take the time to properly check all drain locations, all of the time.
2. Check your fuel tank system to assure it is equipped with raised, umbrella-style fuel filler caps to
preclude water ingress. Inclusion of reduced diameter adapters precludes misfueling also. Be sure the
fuel vent system configuration of the airplane is maintained with any fuel cap selection. Incorrect fuel
cap configuration may lead to reduced fuel flow, bladder collapse, oil-canning in flight, fuel hold-up in
the tank, etc. with consequent engine failure.
1
3. With the airplane in the normal ground attitude and starting at the highest drain location, check all
drain locations for contaminants before every flight, whether or not refueling has occurred. Have fuel
sample disposal provisions, proper lighting, and a small ladder at your disposal to properly check for
fuel tank system contamination.
„F Drain at least one cup of fuel (using a clear sampler cup) from each drain location.
„F Drain the fuel strainer as required to completely flush its contents in each of the fuel selector
positions.
„F Check for water, clarity, cloudiness, haze, proper fuel type/grade (i.e.; 100LL is light blue in tint,
jet fuel is clear or yellowish), odor, or other contaminants.
„F If any contamination is detected in the fuel tank system, thoroughly drain all drain locations
again.
„F If contamination is observed, take further samples until the fuel appears clear, and gently rock
the wings and lower the tail to the ground (or raise the tail and let back down on tail draggers) to
move any additional contaminants to the drain points.
„F Take repeated samples from all drain locations until all contamination has been removed. If
contaminants are still present, do not fly the airplane.
„F Have qualified maintenance personnel drain and purge the fuel tank system. Remove all
evidence of contamination prior to further flight.
4. Take proper precautions to preclude water from entering into your fuel tank system from an external
source (washing, rain, snow, sleet, etc.). Regularly check all external entry sites (caps, access panels, etc.)
for evidence of water ingress into the fuel tank system. When possible store the airplane indoors. If stored
outdoors or exposed to wet conditions (washing, rain, snow, sleet, etc.), examine the fuel tank system
drains for contamination more frequently. Pay particular attention to airplanes that have been externally
cleaned and/or refinished also.
5. During annual or 100-hour inspections do the following:
„F Check fuel caps, cap gaskets, cap adaptors, cap adaptor gaskets, fuel filler neck to adaptor sealer,
fuel gage transmitter gaskets, gage transmitter access covers, and upper surface inspection covers
for condition, proper sealing, security, alignment, etc. Ensure to service and clean these areas,
replacing parts as necessary.
„F Drain and flush the fuel strainer and carburetor bowl completely.
„F Inspect the interior of metal fuel tanks for signs of corrosion, which may indicate water
contamination.
„F Inspect the interior of bladder tanks for wrinkles, broken or missing hangers, etc.
„F If signs of contamination are found, alert the owner and fuel supplier of your findings for
corrective action.
6. Take precautions to preclude water migration in the fuel tank system from an internal source (free water
coming out of solution). Keep fuel tanks full when the airplane will not be operated regularly. Keep fuel
tanks full between flights, provided weight and balance limitations permit. Limit the fuel tanks exposure
to large temperature fluctuations as much as possible. If the airplane has been exposed to sustained wing
low or unusual attitudes or a fuel tank has been run dry, sump contaminants may have migrated
throughout the fuel tank system.
7. Know your fuel supplier. Regularly check and verify quality controls are in place to ensure you receive
only dry, uncontaminated fuel from a supplier. Have on-field checks and verify to ensure continued supply
of dry uncontaminated fuel to an operator. Gain assurance that the fuel supply has been checked for
contamination and is properly filtered before allowing the airplane to be serviced. When ordering fuel,
specifically state the exact fuel grade and quantity needed. Be present at each and every refueling and
observe the fueling process.
2
8. Collect all sampled fuel in a safe container and dispose of properly.
9. Replace all safety items removed during contamination checks. Correct all unsatisfactory conditions
found during or any examination prior to further flight.
For Further Information Contact
Jeff Janusz, Aerospace Engineer, 1801 Airport Road, Rm. 100, Wichita, KS; phone: (316) 946-4148; fax:
(316) 946-4107; e-mail:
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.
Related Advisory and Service Information
Refer to Table I for a list of documents published by FAA, Cessna Aircraft Company, and the
Aircraft Owners and Pilots Association (AOPA) Air Safety Foundation related to fuel tank system
contamination and related issues.
TABLE I
Advisory Circular
Document No. Date Subject Owner
AC 00-34A July 29, 1974 Aircraft Ground Handling and Servicing FAA
AC 20-43C October 10, 1976 Aircraft Fuel Control FAA
AC 20-105B June, 15 1998 Reciprocating Engine Power-Loss Accident Prevention and FAA
Trend Monitoring
AC 20-106 April 1978 Aircraft Inspection for the General Aviation Aircraft Owner FAA
AC 20-122A January 29, 1991 Anti - Misfueling Devices: Their Availability and Use FAA
AC 20-125 December 10, 1985 Water in Aviation Fuels FAA
AC 43.13-1B October, 8 1998 Acceptable Methods, Techniques, and Practices ¡V Aircraft FAA
Inspection and Repair
AC 91-13C July 24, 1979 Cold Weather Operation of Aircraft FAA
AC 150/5230-4A June 18, 2004 Aircraft Fuel Storage, Handling and Dispensing on Airports FAA
Special Airworthiness Information Bulletin
Document No. Date Subject Owner
CE-07-06 October 27, 2006 Alcohol in auto gas FAA
CE-06-06 October, 2005 Steel fuel tanks FAA
CE-05-80 August 9, 2005 Cessna 120 and 140 Fuel Caps FAA
CE-04-11 October 28, 2003 Cessna 182 Series Fuel Caps FAA
CE-03-43R1 September 23, 2003 Cessna 100, 200, 200 and 400 series fuel quantity gauging FAA
Cessna Aircraft Company
Document No. Date Subject Owner
SEB92-23 September 4, 1992 Fuel System Quick Drain Modification Cessna
SEB92-24 September 4, 1992 Fuel System Quick Drain Valve Installation Cessna
SEB92-25 September 4, 1992 Fuel System Quick Drain Valve Installation Cessna
SEB92-26 September 4, 1992 Additional Fuel Tank Drain Valves Installation Cessna
SEB 92-27 September 4, 1992 Raised Reduced Diameter Fuel Cap Installation Cessna
SE70-28 October 23, 1970 Fuel Tank Filler Neck Sealing Cessna
SE69-15 July 18, 1969 Fuel Tank Quick Drain Valves Cessna
SNL98-9 October 26, 1998 Pilot Safety and Warning Supplements Cessna
D5139-13 June 1, 1998 Pilot Safety and Warning Supplements (Reissue) Cessna
SNL85-53 November 27, 1985 Pilot Safety and Warning Supplements Cessna
D5139-13 October 2, 1985 Pilot Safety and Warning Supplements (Orig. Issue) Cessna
SE82-36 July 30, 1982 Fuel Contamination Cessna
SE80-87 October 27, 1980 Fuel Contamination Cessna
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Aircraft Owners and Pilots Association (AOPA) Air Safety Foundation
Document No. Date Subject Owner
Safety Advisor Operations and Fuel Awareness AOPA
Proficiency No. 5
Safety Brief No. 4 Misfueling AOPA
4
Dan Weiler
Executive Director of the Cessna Owner Organization
(715) 445-5000, ext. 116
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