Sent: Wednesday, December 29, 2004 3:31
PM
Subject: ALERT TO PILOTS: WING UPPER
SURFACE ICE ACCUMULATION
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NTSB ADVISORY
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National Transportation Safety Board
Washington, DC 20594
December 29, 2004
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ALERT TO PILOTS: WING UPPER SURFACE ICE ACCUMULATION
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As a result of a recent takeoff accident that has generated much
discussion about the effects of wing upper surface ice
accumulations, the National Transportation Safety Board is
issuing the following alert letter to pilots:
Wing Upper Surface Ice
Accumulation Alert
The National Transportation Safety Board has long been concerned
about the insidious nature of the effects of small amounts of
ice accumulated on an airplane's upper wing surface. The Safety
Board's preliminary investigation of the November 28, 2004
accident involving a Bombardier Challenger 604 in Montrose,
Colorado,(1) has revealed that atmospheric conditions conducive
to upper wing surface ice accumulation existed at the time of
the accident (airplane performance issues, including the
possibility of upper wing ice contamination, are being
investigated).
For years most pilots have understood that visible ice
contamination on a wing can cause severe aerodynamic and control
penalties; however, it has become apparent that many pilots do
not recognize that minute amounts of ice adhering to a wing can
result in similar penalties. Research results have shown that
fine particles of frost or ice, the size of a grain of table
salt and distributed as sparsely as one per square centimeter
over an airplane wing's upper surface can destroy enough lift to
prevent that airplane from taking off. The Safety Board has
commented on the hazards of upper wing ice accumulation in
several previous aircraft accident reports;
some excerpts from these reports follow:
(1) -- According to wind-tunnel data, a wing upper surface
roughness caused by particles of only 1-2 mm [millimeter]
diameter [the size of a grain of table salt], at a density of
about one particle per square centimeter, can cause lift losses
of about 22 and 33 percent, in ground effect and free air,
respectively.(2) -- Research has
shown that almost imperceptible amounts of ice on an airplane's
wing upper surface during takeoff can result in significant
performance degradation.
Therefore, the Safety Board has urged pilots to conduct visual
and tactile inspections of airplane wing upper surfaces in past
safety recommendations (including Safety Recommendation A-04-66,
which was issued to the FAA on December 15, 2004).
(3) -- Ice accumulation on the wing upper
surface is very difficult to detect. It may not be seen from the
cabin because it is clear/white and it is very difficult to see
from the front or back of the wing. The Safety Board believes
strongly that the only way to ensure that the wing is free from
critical contamination is to touch it.
(4) -- Accident history shows that
non-slatted, turbojet, transport-category airplanes have been
involved in a disproportionate number of takeoff accidents where
undetected upper wing ice contamination has been cited as the
probable cause or sole contributing factor.
(5) -- The industry acknowledges that it is
nearly impossible to determine by observation whether a wing is
wet or has a thin film of ice. A very thin film of ice or frost
will degrade the aerodynamic performance of any airplane.
(6) -- The Safety Board believes
that even with the wing inspection light, the observation of a
wing from a 30- to 40-foot distance, through a window that was
probably wet from precipitation, does not constitute a careful
examination. The Safety Board acknowledges that the detection of
minimal amounts of contamination, sufficient to cause
aerodynamic performance problems, is difficult and may not be
possible without a tactile inspection.
(7) -- The Federal Aviation
Administration's (FAA) Environmental Icing National Resource
Specialist (NRS) indicated that he was concerned that most
pilots were not aware that a slight amount of frost or ice
accumulation could result in a significant degradation of
airplane performance. The Icing NRS stated, 'pilots may observe
what they perceive to be an insignificant amount of ice on the
airplane's surface and be unaware that they may still be at risk
because of reduced stall margins resulting from icing-related
degraded airplane performance.'
(8) -- From an aerodynamic viewpoint, there
is no such thing as "a little ice." Strict attention should be
focused on ensuring that critical aircraft surfaces are free of
ice
contamination at the initiation of takeoff.
(9) -- Strange as it may seem, a very light
coating of snow or ice, light enough to be hardly visible, will
have a tremendous effect on reducing the performance of a modern
airplane. (Jerome Lederer, M.E., 1939)
(10) Despite the accident and research
evidence indicating that small, almost visually imperceptible
amounts of ice accumulation on the upper surface of a wing can
cause the same aerodynamic penalties as much larger (and more
visible) ice accumulations, recent accidents indicate that the
pilot community still may not appreciate the potential
consequences of small amounts of ice. For example, see the
final report on the October 10, 2001, accident involving the
Cessna 208, N9530F that occurred in Dillingham, Alaska; (11)
also see the final report on the January 4, 2002, accident
involving the Bombardier Challenger 604, N90AG, which occurred
in Birmingham, England.
(12) It appears that some pilots believe
that if they cannot see ice or frost on the wing from a
distance, or maybe through a cockpit or cabin window, it must
not be there - or if it is there and they cannot see it under
those circumstances, then the accumulation must be too minute to
be of any consequence. Despite evidence to the contrary, these
beliefs may still exist because many pilots have seen their
aircraft operate with large amounts of ice adhering to the
leading edges (including the dramatic double horn accretion) and
consider a thin layer of ice or frost on the wing upper surface
to be more benign. However, as noted, research has shown that
small amounts of ice accumulation on the upper surface of a wing
can result in aerodynamic degradation as severe as that caused
by much larger (and more visible) ice accumulations.
It is also possible that many pilots believe that if they have
sufficient engine power available, they can simply "power
through" any performance degradation that might result from
almost imperceptible amounts of upper wing surface ice
accumulation. However, engine power will not prevent a stall
and loss of control at lift off, where the highest angles of
attack are normally achieved. Further, small patches of almost
imperceptible ice or frost can result in localized, asymmetrical
stalls on the wing, which can result in roll control problems
during lift off.
The Safety Board notes that there are circumstances in which
upper wing surface ice accumulation can be difficult to perceive
visually. For example, depending on the airplane's design
(size, high wing, low wing, etc.) and the environmental and
lighting conditions (wet wings, dark night, dim lights, etc.) it
may be difficult for a pilot to see ice on the upper wing
surface from the ground or through the cockpit or other
windows. Further, frost, snow, and rime ice can be very
difficult to detect on a white upper wing surface and clear ice
can be difficult to detect on an upper wing surface of any
color. However, it is critically important to ensure, by any
means necessary, that the upper wing surface is clear of
contamination before takeoff. That is why the Safety Board
recently issued Safety Recommendation A-04-66, urging pilots to
conduct visual and tactile inspections of airplane wing upper
surfaces.
The bottom line is that pilots should be aware that no amount of
snow, ice or frost accumulation on the wing upper surface can be
considered safe for takeoff. However, history has shown that
with a careful and thorough preflight inspection, including
tactile inspections and proper and liberal use of deicing
processes and techniques, airplanes can be operated safely in
spite of the adversities encountered during winter months.
(1) Additional information regarding this accident can be found
on the Safety Board's Web site at
http://www.ntsb.gov,
accident number DEN05MA028.
(2) This information is from the Safety Board's final report on
the March 22, 1992, accident involving USAir flight 405, at
Flushing, New York. For additional information, see National
Transportation Safety Board. 1993. Takeoff Stall in Icing
Conditions, USAir flight 405, Fokker F-28, N485US, LaGuardia
Airport, Flushing, New York, March 22, 1992. Aircraft Accident
Report NTSB/AAR-93/02. Washington, D.C.
(3) For additional information, see
http://www.ntsb.gov/recs/letters/2004/A04_64_67.pdf.
(4) This information is from the Safety Board's final report on
the February 17, 1991, accident involving Ryan International
Airlines, at Cleveland, Ohio. For additional
information, see National Transportation Safety Board. 1991.
Ryan International Airlines, DC-9-15, N565PC, Loss of Control
on Takeoff, Cleveland-Hopkins International Airport, Cleveland,
Ohio, February 17, 1991. Aircraft Accident Report
NTSB/AAR-91/09. Washington, D.C.
(5) See Aircraft Accident Report NTSB/AAR-93/02. Washington,
D.C., cited above.
(6) See Aircraft Accident Report NTSB/AAR-93/02. Washington,
D.C., cited above.
(7) See Aircraft Accident Report NTSB/AAR-93/02. Washington,
D.C., cited above.
(8) This is information contained in the Safety Board's final
Report on the January 9, 1997, accident involving Comair flight
3272 at Monroe, Michigan. For additional information, see
National Transportation Safety Board. 1998. In-flight Icing
Encounter and Uncontrolled Collision with Terrain, Comair flight
3272, Embraer EMB-120RT, N265CA, Monroe, Michigan, January 9,
1997. Aircraft Accident Report NTSB/AAR-98/04. Washington,
D.C.
(9) This statement is a quote from a technical paper, titled,
The Effect of Wing Ice Contamination on Essential Flight
Characteristics, by Douglas Aircraft Company's deputy
chief design engineer for the MD-80/DC-9 program (presented in
1988 and again in 1991). See appendix E of the previously cited
Aircraft Accident Report NTSB/AAR-91/09.
(10) This quote is from Safety in the Operation of Air
Transportation, a lecture presented by Jerome Lederer, M.E., at
Norwich University, in 1939, and cited in the Safety
Board's final report on the March 22, 1992, accident involving
USAir flight 405 at Flushing, New York. See Aircraft Accident
Report NTSB/AAR-93/02. Washington, D.C., cited above.
(11) As a result of this and other icing-related accidents
involving Cessna 208 series airplanes, on December 15, 2004, the
Safety Board issued Safety Recommendations A-04-64 through
-67. Additional information on the Dillingham, Alaska accident
(DCA02MA003) and on Safety Recommendations A-04-64 through -67
can be found on the Safety Board's Web site at
http://www.ntsb.gov.
(12) This accident was investigated by the Air Accidents
Investigation Branch (AAIB), Department for Transport, Great
Britain. Additional information on this accident can be found
at
www.dft.gov.uk/stellent/groups.dft_avsafety/documents/page/dft_avsafety_030576.hcsp
(Although broader than the issue of wing upper surface
ice accumulation discussed in this alert notice, aircraft icing
has been an issue on the NTSB's Most Wanted List of
Safety Improvements since 1997. A summary of the Board's actions
and recommendations in this area may be found on its website, at
www.ntsb.gov/Recs/mostwanted/air_ice.htm.)
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NTSB Media Contact: Ted Lopatkiewicz
(202) 314-6100
lopatt@ntsb.gov
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