[Federal Register Volume 61, Number 89 (Tuesday, May 7, 1996)]
[Rules and Regulations]
[Pages 20639-20641]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 96-10722]
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DEPARTMENT OF TRANSPORTATION
14 CFR Part 39
[Docket No. 96-CE-04-AD; Amendment 39-9590; AD 96-09- 14]
RIN 2120-AA64
Airworthiness Directives; Dornier 228 Series Airplanes
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule.
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SUMMARY: This amendment adopts a new airworthiness directive (AD) that
applies to all Dornier 228 series airplanes. This action requires
revising the Airplane Flight Manual (AFM) to provide the flight crew
with recognition cues for, and procedures for exiting from, severe
icing conditions, and to
[[Page 20640]]
limit or prohibit the use of various flight control devices. This
amendment is prompted by results of a review of the requirements for
certification of the airplane in icing conditions, new information on
the icing environment, and icing data provided currently to the flight
crews. The actions specified by this AD are intended to minimize the
potential hazards associated with operating the airplane in freezing
rain or freezing drizzle conditions by providing more clearly defined
procedures and limitations associated with such conditions.
EFFECTIVE DATE: June 11, 1996.
ADDRESSES: Information that relates to this AD may be examined at the
Federal Aviation Administration (FAA), Central Region, Office of the
Assistant Chief Counsel, Attention: Rules Docket 96-CE-04-AD, Room
1558, 601 E. 12th Street, Kansas City, Missouri 64106.
FOR FURTHER INFORMATION CONTACT: Mr. John Dow, Aerospace Engineer, FAA,
Small Airplane Directorate, 1201 Walnut, suite 900, Kansas City,
Missouri 64106; telephone (816) 426-6934; facsimile (816) 426-2169.
SUPPLEMENTARY INFORMATION: A proposal to amend part 39 of the Federal
Aviation Regulations (14 CFR part 39) to include an AD that would apply
to Dornier 228 series airplanes was published in the Federal Register
on January 25, 1996 (61 FR 2172). The action proposed to require
revising the Airplane Flight Manual (AFM) to specify procedures that
would prohibit flight in freezing rain or freezing drizzle conditions
(as determined by certain visual cues), limit or prohibit the use of
various flight control devices, and provide the flight crew with
recognition cues for, and procedures for exiting from, severe icing
conditions.
Disposition of Comments
For the disposition of comments on this rulemaking action, see
Docket No. 96-CE-01; Amendment 39-9587; AD 96-09-11, Airworthiness
Directives; de Havilland, Inc. DHC-6 Series Airplanes, published
elsewhere in this issue of the Federal Register.
Conclusion
After careful review of the available data, including the comments
noted above, the FAA has determined that air safety and the public
interest require the adoption of the rule with the changes previously
described. The FAA has determined that these changes will neither
increase the economic burden on any operator nor increase the scope of
the AD.
Cost Impact
The FAA estimates that 169 airplanes in the U.S. registry will be
affected by this AD, that it will take approximately 1 workhour per
airplane to accomplish the required action, and that the average labor
rate is approximately $60 an hour. Since an owner/operator who holds at
least a private pilot's certificate as authorized by sections 43.7 and
43.11 of the Federal Aviation Regulations (14 CFR 43.7 and 43.11) can
accomplish the required action, the only cost impact upon the public is
the time it would take the affected airplane owner/operators to
incorporate the AFM revisions.
In addition, the FAA recognizes that this AD may impose operational
costs. However, those costs are incalculable because the frequency of
occurrence of the specified conditions and the associated additional
flight time cannot be determined. Nevertheless, because of the severity
of the unsafe condition addressed, the FAA has determined that
continued operational safety necessitates the imposition of these
costs.
Regulatory Impact
The regulations adopted herein will not have substantial direct
effects on the States, on the relationship between the national
government and the States, or on the distribution of power and
responsibilities among the various levels of government. Therefore, in
accordance with Executive Order 12612, it is determined that this final
rule does not have sufficient federalism implications to warrant the
preparation of a Federalism Assessment.
For the reasons discussed above, I certify that this action (1) is
not a ``significant regulatory action'' under Executive Order 12866;
(2) is not a ``significant rule'' under DOT Regulatory Policies and
Procedures (44 FR 11034, February 26, 1979); and (3) will not have a
significant economic impact, positive or negative, on a substantial
number of small entities under the criteria of the Regulatory
Flexibility Act. A copy of the final evaluation prepared for this
action is contained in the Rules Docket. A copy of it may be obtained
by contacting the Rules Docket at the location provided under the
caption ADDRESSES.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
Adoption of the Amendment
Accordingly, pursuant to the authority delegated to me by the
Administrator, the Federal Aviation Administration amends part 39 of
the Federal Aviation Regulations (14 CFR part 39) as follows:
PART 39--AIRWORTHINESS DIRECTIVES
1. The authority citation for part 39 continues to read as follows:
Authority: 49 USC 106(g), 40113, 44701.
Sec. 39.13 [Amended]
2. Section 39.13 is amended by adding a new airworthiness directive
(AD) to read as follows:
96-09-14 Dornier: Amendment 39-9590; Docket No. 96- CE-04-AD.
Applicability: Models 228-100, 228-101, 228-200, 228- 201, 228-202,
and 228-212 airplanes (all serial numbers), certificated in any
category.
Note 1: This AD applies to each airplane identified in the
preceding applicability provision, regardless of whether it has been
modified, altered, or repaired in the area subject to the
requirements of this AD. For airplanes that have been modified,
altered, or repaired so that the performance of the requirements of
this AD is affected, the owner/operator must request approval for an
alternative method of compliance in accordance with paragraph (d) of
this AD. The request should include an assessment of the effect of
the modification, alteration, or repair on the unsafe condition
addressed by this AD; and, if the unsafe condition has not been
eliminated, the request should include specific proposed actions to
address it.
Compliance: Required as indicated, unless accomplished
previously.
To minimize the potential hazards associated with operating the
airplane in severe icing conditions by providing more clearly
defined procedures and limitations associated with such conditions,
accomplish the following:
(a) Within 30 days after the effective date of this AD,
accomplish the requirements of paragraphs (a)(1) and (a)(2) of this
AD.
Note 2: Operators must initiate action to notify and ensure that
flight crewmembers are apprised of this change.
(1) Revise the FAA-approved Airplane Flight Manual (AFM) by
incorporating the following into the Limitations Section of the AFM.
This may be accomplished by inserting a copy of this AD in the AFM.
``WARNING
Severe icing may result from environmental conditions outside of
those for which the airplane is certificated. Flight in freezing
rain, freezing drizzle, or mixed icing conditions (supercooled
liquid water and ice crystals) may result in ice build-up on
protected surfaces exceeding the capability of the ice protection
system, or may result in ice forming aft of the protected surfaces.
This ice may not be shed using the ice protection systems, and may
seriously degrade the performance and controllability of the
airplane.
[[Page 20641]]
During flight, severe icing conditions that exceed
those for which the airplane is certificated shall be determined by
the following visual cues. If one or more of these visual cues
exists, immediately request priority handling from Air Traffic
Control to facilitate a route or an altitude change to exit the
icing conditions.
--Unusually extensive ice accreted on the airframe in areas not
normally observed to collect ice.
--Accumulation of ice on the upper surface of the wing aft of the
protected area.
--Accumulation of ice on the propeller spinner farther aft than
normally observed.
Since the autopilot may mask tactile cues that indicate
adverse changes in handling characteristics, use of the autopilot is
prohibited when any of the visual cues specified above exist, or
when unusual lateral trim requirements or autopilot trim warnings
are encountered while the airplane is in icing conditions.
All icing detection lights must be operative prior to
flight into icing conditions at night. [NOTE: This supersedes any
relief provided by the Master Minimum Equipment List (MMEL).]''
(2) Revise the FAA-approved AFM by incorporating the following
into the Procedures Section of the AFM. This may be accomplished by
inserting a copy of this AD in the AFM.
``THE FOLLOWING WEATHER CONDITIONS MAY BE CONDUCIVE TO SEVERE IN-FLIGHT
ICING:
Visible rain at temperatures below 0 degrees Celsius
ambient air temperature.
Droplets that splash or splatter on impact at
temperatures below 0 degrees Celsius ambient air temperature.
PROCEDURES FOR EXITING THE SEVERE ICING ENVIRONMENT:
These procedures are applicable to all flight phases from
takeoff to landing. Monitor the ambient air temperature. While
severe icing may form at temperatures as cold as -18 degrees
Celsius, increased vigilance is warranted at temperatures around
freezing with visible moisture present. If the visual cues specified
in the Limitations Section of the AFM for identifying severe icing
conditions are observed, accomplish the following:
Immediately request priority handling from Air Traffic
Control to facilitate a route or an altitude change to exit the
severe icing conditions in order to avoid extended exposure to
flight conditions more severe than those for which the airplane has
been certificated.
Avoid abrupt and excessive maneuvering that may
exacerbate control difficulties.
Do not engage the autopilot.
If the autopilot is engaged, hold the control wheel
firmly and disengage the autopilot.
If an unusual roll response or uncommanded roll control
movement is observed, reduce the angle-of-attack.
Do not extend flaps during extended operation in icing
conditions. Operation with flaps extended can result in a reduced
wing angle-of-attack, with the possibility of ice forming on the
upper surface further aft on the wing than normal, possibly aft of
the protected area.
If the flaps are extended, do not retract them until
the airframe is clear of ice.
Report these weather conditions to Air Traffic
Control.''
(b) Incorporating the AFM revisions, as required by this AD, may
be performed by the owner/operator holding at least a private pilot
certificate as authorized by section 43.7 of the Federal Aviation
Regulations (14 CFR 43.7), and must be entered into the aircraft
records showing compliance with this AD in accordance with section
43.11 of the Federal Aviation Regulations (14 CFR 43.11).
(c) Special flight permits may be issued in accordance with
sections 21.197 and 21.199 of the Federal Aviation Regulations (14
CFR 21.197 and 21.199) to operate the airplane to a location where
the requirements of this AD can be accomplished.
(d) An alternative method of compliance or adjustment of the
compliance time that provides an acceptable level of safety may be
used if approved by the Manager, Small Airplane Directorate, FAA,
1201 Walnut, suite 900, Kansas City, Missouri 64106. The request
shall be forwarded through an appropriate FAA Maintenance Inspector,
who may add comments and then send it to the Manager, Small Airplane
Directorate.
Note 3: Information concerning the existence of approved
alternative methods of compliance with this AD, if any, may be
obtained from the Small Airplane Directorate.
(e) All persons affected by this directive may examine
information related to this AD at the FAA, Central Region, Office of
the Assistant Chief Counsel, Room 1558, 601 E. 12th Street, Kansas
City, Missouri 64106.
(f) This amendment (39-9590) becomes effective on June 11, 1996.
Issued in Kansas City, Missouri, on April 24, 1996.
Henry A. Armstrong,
Acting Manager, Small Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 96-10722 Filed 5-1-96; 3:24 am]
BILLING CODE 4910-13-P
