Airworthiness Directives; Raytheon Aircraft Company Beech 17, 18, 19, 23, 24, 33, 35, 36/A36, A36TC/B36TC, 45, 50, 55, 56, 58, 58P, 58TC, 60, 65, 70, 76, 77, 80, 88, and 95 Series Airplanes
Requires installing a placard on the fuel tank selector to warn of the no-flow condition that exists between the fuel tank detents.
[Federal Register Volume 65, Number 134 (Wednesday, July 12, 2000)]
[Rules and Regulations]
[Pages 42855-42856]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 00-17622]
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Federal Register / Vol. 65, No. 134 / Wednesday, July 12, 2000 /
Rules and Regulations
[[Page 42855]]
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 98-CE-61-AD; Amendment 39-11061; AD 99-05-13]
RIN 2120-AA64
Airworthiness Directives; Raytheon Aircraft Company Beech 17, 18,
19, 23, 24, 33, 35, 36/A36, A36TC/B36TC, 45, 50, 55, 56, 58, 58P, 58TC,
60, 65, 70, 76, 77, 80, 88, and 95 Series Airplanes
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule; withdrawal.
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SUMMARY: This amendment withdraws Airworthiness Directive (AD) 99-05-
13, which currently applies to Raytheon Aircraft Company (Raytheon)
Beech 17, 18, 19, 23, 24, 33, 35, 36/A36, A36TC/B36TC, 45, 50, 55, 56,
58, 58P, 58TC, 60, 65, 70, 76, 77, 80, 88, and 95 series airplanes. AD
99-05-13 requires installing a placard on the fuel tank selector to
warn of the no-flow condition that exists between the fuel tank
detents. Since the issuance of AD 99-05-13, the Federal Aviation
Administration (FAA) has re-evaluated all information related to this
subject, and determined that the subject matter in this AD is an
operational issue and does not address an unsafe condition.
Accordingly, this action withdraws AD 99-05-13.
FOR FURTHER INFORMATION CONTACT: Mr. Jeff Pretz, Aerospace Engineer,
Wichita Aircraft Certification Office, FAA, 1801 Airport Road, Mid-
Continent Airport, Wichita, Kansas 67209; telephone: (316) 946-4153;
facsimile: (316) 946-4407.
SUPPLEMENTARY INFORMATION:
Discussion
Has FAA Taken Any Action to This Point?
Reports of engine stoppage on Raytheon Beech 17, 18, 19, 23, 24,
33, 35, 36/A36, A36TC/B36TC, 45, 50, 55, 56, 58, 58P, 58TC, 60, 65, 70,
76, 77, 80, 88, and 95 series airplanes caused FAA to issue AD 99-05-
13, Amendment 39-11061 (64 FR 10560, March 5, 1999). AD 99-05-13
currently requires installing a placard on the fuel tank selector to
warn of the no-flow condition that exists between the fuel tank
detents.
After issuing AD 99-05-13, we re-evaluated all information related
to the subject matter of this AD and determined that:
The positioning of the fuel selector is an operational
issue and not an unsafe condition under part 39 of the Federal Aviation
Regulations (14 CFR part 39) and should be handled by other methods;
Normal operating and procedural information such as this
should be handled through regular revisions to the Airplane Flight
Manual (AFM) or Pilot's Operating Handbook (POH); and
Issuing an AD to require a placard that conveys normal
operating information reduces the pilots' sensitivity to true emergency
information that should be conveyed by placards.
Consequently, FAA issued a proposal to amend part 39 of the Federal
Aviation Regulations (14 CFR part 39) to withdraw AD 99-05-13. This
proposal published in the Federal Register as a notice of proposed
rulemaking (NPRM) on March 30, 2000 (65 FR 16845).
Was the Public Invited to Comment?
The FAA invited interested persons to participate in the making of
this amendment. The following describes each comment and presents FAA's
response.
Comment Issue No. 1: AD is Valid if an Unsafe Condition Exists
What is the Commenter's Concern?
One commenter states that FAA is withdrawing this AD because it is
an operational issue and should be handled by other methods. The
commenter believes that the AD is valid because FAA has the authority
to issue an AD on any issue as long as an unsafe condition exists.
What is FAA's Response to the Concern?
We concur that we have the authority and responsibility to act on
an unsafe condition, regardless of the factors that create the unsafe
condition. We were in error in including information in the NPRM
specifying that an operational procedure cannot be the subject of an
AD. However, we determined that the fuel selector valve, when
functioning properly and used properly, does not create an unsafe
condition. The FAA determined that the procedures to operate the fuel
selector valve are readily available and that our authority is not to
issue AD's against aircraft where the operators do not operate the
equipment correctly. Utilizing positive detent to assure that the fuel
valve is fully open to the tank selected is considered a standard
design practice in the aircraft industry.
We are not changing the AD action as a result of this comment.
Comment Issue No. 2: AD is Needed for Airplanes Without an AFM/POH
What is the Commenter's Concern?
One commenter states that many airplanes currently affected by AD
99-05-13 are not required to have a POH, and Civil Aviation Regulations
(CAR) part 3 allows a manufacturer to use placards instead of an AFM.
The commenter believes that, for these reasons, the AD is valid.
What is FAA's Response to the Concern?
We concur that many aircraft do not require a POH and were
certificated under CAR part 3 where the use of placards is acceptable
over an AFM. However, airplanes in this situation usually only have
placards installed that contain safety information when an unusual
design, operating, or handling characteristic is prevalent.
The FAA has the authority to issue an AD to require operational
placards. However, as discussed above, utilizing a positive detent to
assure that the fuel valve is fully open to the tank selected is
considered a standard design practice in the aircraft industry.
We are not changing the AD action as a result of this comment.
Comment Issue No. 3: Placards Are Necessary to Convey Safe
Operation
What is the Commenter's Concern?
One commenter states that the AD is valid because placards are
necessary to
[[Page 42856]]
convey safe operation for airplanes certificated under the Civil
Aviation Regulations and part 23 of the Federal Aviation Regulations
(14 CFR part 23). The commenter also states that placards should not be
limited to only emergency information.
What is FAA's Response to the Concern?
We concur that placards are not just limited to emergency
information. All required placards should convey information for safe
operation. However, both CAR 3.777/3.777-1 and 14 CFR 23.1541 state
that placards should convey safe operation information if the aircraft
has unusual design, operation, or handling characteristics. As
discussed previously, utilizing a positive detent to assure that the
fuel valve is fully open to the tank selected is considered a standard
design practice in the aircraft industry.
We are not changing the AD action as a result of this comment.
Comment Issue No. 4: FAA Has Changed the Definition of Unsafe
Condition
What is the Commenter's Concern?
One commenter states that, by withdrawing AD 99-05-13, FAA will
have changed the historical definition of an unsafe condition. We infer
that the commenter wants to maintain the effectiveness of AD 99-05-13.
What is FAA's Response to the Concern?
We do not concur that we have altered the definition of an unsafe
condition. Determination of an unsafe condition is based on each
individual situation. Factors that are considered include the design,
operation, or handling characteristics of the type design airplanes. As
discussed above, utilizing a positive detent to assure that the fuel
valve is fully open to the tank selected is considered a standard
design practice in the aircraft industry.
We are not changing the AD action as a result of this comment.
Comment Issue No. 5: Numerous Occurrences Justify the Current AD
What is the Commenter's Concern?
One commenter states that placing a warning placard specifying the
safe operation of the fuel selector as AD 99-05-13 requires supports
the 49 occurrences from the records of the National Transportation
Safety Board (NTSB). We infer that the commenter wants to maintain the
effectiveness of AD 99-05-13.
What is FAA's Response to the Concern?
We do not concur with the commenter's assessment. We have reviewed
37 reports of the above-referenced 49 occurrences (commenter only
provided 37). Approximately half of the occurrences listed the cause as
fuel starvation in combination with the fuel selector not positioned in
the detent. The most prevalent cause was failure to follow checklist
procedures. In no instance was the pilot's lack of knowledge or
understanding of the positioning of the fuel selector listed as the
cause of the occurrence.
In addition, NTSB has not recommended that FAA issue an AD on this
subject. Therefore, we conclude that the commenter believes NTSB
supports the placard requirement, when in fact, NTSB has made no
recommendation supporting it. Again, utilizing a positive detent to
assure that the fuel valve is fully open to the tank selected is
considered a standard design practice in the aircraft industry.
We are not changing the AD action as a result of this comment.
The FAA's Determination
What is FAA's Final Determination on This Issue?
Based on the above information, FAA has determined that there is no
need for AD 99-05-13 and that it should be withdrawn.
This action withdraws AD 99-05-13. Withdrawal of AD 99-05-13 will
not preclude us from issuing another notice in the future, nor will it
commit us to any course of action in the future.
Regulatory Impact
Since this action only withdraws an AD, it is not an AD and,
therefore, is not covered under Executive Order 12866, the Regulatory
Flexibility Act, or DOT Regulatory Policies and Procedures (44 FR
11034, February 26, 1979).
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Safety.
The Withdrawal
Accordingly, FAA withdraws AD 99-05-13, Amendment 39-11061 (64 FR
10560, March 5, 1999).
Issued in Kansas City, Missouri, on July 5, 2000.
Michael Gallagher,
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 00-17622 Filed 7-11-00; 8:45 am]
BILLING CODE 4910-13-U
Sources. Section 1 is written by AircraftDirectives from the record below and is a reading aid only. Section 2 is the United States Government's own text, reproduced without edit.
Federal Register: https://www.federalregister.gov/documents/2000/07/12/00-17622/airworthiness-directives-raytheon-aircraft-company-beech-17-18-19-23-24-33-35-36a36-a36tcb36tc-45-50
Official PDF: https://www.govinfo.gov/content/pkg/FR-2000-07-12/pdf/00-17622.pdf
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