FOR IMMEDIATE RELEASE: August 27, 1998 SB-98-32
SAFETY BOARD FAULTS FAA AIRCRAFT CERTIFICATION STANDARDS AND
OVERSIGHT IN MICHIGAN COMMUTER AIRLINER CRASH
Washington, D.C. - The National Transportation Safety Board today
determined that the probable cause of a commuter aircraft accident
near Monroe, Michigan was the FAA's failure to establish adequate
aircraft certification standards for flight in icing conditions.
Also cited was the FAA's failure to ensure that approved procedures
for deicing system operation were implemented by U.S. air carriers,
and to require the establishment of adequate minimum airspeeds
for icing conditions, which led to a loss of control when the
airplane accumulated a thin, rough accretion of ice on the wings.
Contributing to the accident, the Board found, were the flightcrew's
decision to operate in icing conditions near the lower margin
of the operating airspeed envelope (with flaps retracted), and
Comair's failure to establish and adequately disseminate unambiguous
minimum airspeed values for flap configurations and flight in
icing conditions.
The accident occurred on January 9, 1997, when Comair flight 3272,
an Embraer 120RT aircraft, crashed while on approach to Detroit
Metropolitan Wayne County Airport. All 26 passengers and three
crewmembers on board were killed and the aircraft was destroyed.
The Board's investigation revealed that, despite the accumulated
lessons of several major accidents, the FAA failed to adopt a
systematic, proactive approach to the certification and operational
issues of turboprop aircraft icing. The icing certification process
was found to be inadequate because it does not require manufacturers
to demonstrate the airplane's flight handling characteristics
under a sufficiently realistic range of adverse ice accretion/flight
handling conditions. Additionally, the Board was critical of FAA
policies that allow an air carrier to elect not to adopt the manufacturer's
changes to the airplane flight manual. This, the Board said, can
result in carriers using procedures that may not reflect the safest
operating practices.
The Board noted that, consistent with Comair's procedures, the
pilots did not activate the leading edge deicing boots during
their descent and approach to the airport because they likely
did not perceive that the airplane was accreting significant structural
ice. Had they been aware of the circumstances of six previous
EMB-120 icing accidents, and a relevant revision to the airplane
flight manual by the manufacturer, it is possible that they would
have operated the airplane more conservatively with regard to
airspeed and flap configuration or activated the deicing boots
when they knew they were in icing conditions.
Because the pilots were operating with the autopilot engaged during
a series of descents, turns, and power and airspeed adjustments,
they may not have perceived the airplane's gradually deteriorating
performance. The Board stressed that disengagement of the autopilot
while flying in icing conditions will enable pilots to sense the
aerodynamic effects of ice accretion and enhance their ability
to retain control of the aircraft.
The Board found that current operating procedures recommending
that pilots wait until ice accumulates to an observable thickness
before activating deicing boots results in unnecessary exposure
to a significant risk for turboprop aircraft. Based primarily
on concerns about ice-bridging, pilots continue to use procedures
that increase the likelihood of potentially hazardous degraded
airplane performance resulting from small amounts of rough ice
on the leading edges.
As a result of this investigation, the Board made 19 recommendations
to the FAA to remedy the problems that have been uncovered. Included
was a recommendation that, jointly with NASA and other interested
aviation organizations, the FAA organize an industry-wide training
effort to educate manufacturers, operators and pilots of turboprop
aircraft regarding the hazards of thin, possibly imperceptible,
rough ice accumulations, the importance of activating deicing
boots on entering icing conditions, and the necessity of maintaining
minimum airspeeds in icing conditions.
In addition, the Board reiterated a 1996 recommendation calling
on the FAA to revise icing certification testing regulations to
ensure that airplanes are properly tested for all conditions in
which they are authorized to operate, or are otherwise shown to
be capable of safe flight into such conditions. If safe operations
cannot be demonstrated by the manufacturer, operational limitations
should be imposed to prohibit flight in such conditions and flightcrews
should be provided with the means to positively determine when
they are in icing conditions that exceed the limits for aircraft
certification.
The NTSB's complete report on this accident, PB98-910404, may
be purchased from the National Technical Information Service,
5285 Port Royal Road, Springfield, VA 22161, (703) 487-4650. The
report also will be placed on the Board's web page (www.ntsb.gov)
in the near future.
NTSB Media Contact: Paul Schlamm
(202) 314-6100