[Federal Register Volume 63, Number 121 (Wednesday, June 24, 1998)]
[Rules and Regulations]
[Pages 34268-34269]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 98-16493]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 97-NM-302-AD; Amendment 39-10621; AD 98-13-30]
RIN 2120-AA64


Airworthiness Directives; Gulfstream Aerospace Corporation Model 
G-159 (G-I) Airplanes

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule.

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SUMMARY: This amendment adopts a new airworthiness directive (AD), 
applicable to all Gulfstream Aerospace Corporation Model G-159 (G-I) 
airplanes, that requires revising the Airplane Flight Manual (AFM) to 
prohibit positioning the power levers below the flight idle stop. This 
amendment is prompted by incidents and accidents involving airplanes 
equipped with turboprop engines in which the ground propeller beta 
range was used improperly during flight. The actions specified by this 
AD are intended to prevent loss of airplane controllability or engine 
overspeed with consequent loss of engine power caused by the power 
levers being positioned below the flight idle stop while the airplane 
is in flight.

EFFECTIVE DATE: July 29, 1998.

ADDRESSES: Information pertaining to this rulemaking action may be 
examined at the Federal Aviation Administration (FAA), Transport 
Airplane Directorate, Rules Docket, 1601 Lind Avenue, SW., Renton, 
Washington; or at the FAA, Small Airplane Directorate, Atlanta Aircraft 
Certification Office, 1895 Phoenix Boulevard, suite 450, Atlanta, 
Georgia.

FOR FURTHER INFORMATION CONTACT: Wayne A. Shade, Aerospace Engineer, 
Airframe and Propulsion Branch, ACE-117A , FAA, Small Airplane 
Directorate, Atlanta Aircraft Certification Office, 1895 Phoenix 
Boulevard, suite 450, Atlanta, Georgia 30349; telephone (770) 703-7337; 
fax (770) 703-6097.

SUPPLEMENTARY INFORMATION: A proposal to amend part 39 of the Federal 
Aviation Regulations (14 CFR part 39) to include an airworthiness 
directive (AD) that is applicable to all Gulfstream Aerospace 
Corporation Model G-159 (G-I) airplanes was published in the Federal 
Register on April 27, 1998 (63 FR 20556). That action proposed to 
require revising the Limitations Section of the Airplane Flight Manual 
(AFM) to prohibit the positioning of the power

[[Page 34269]]

levers below the flight idle stop while the airplane is in flight, and 
to add a statement of the consequences of positioning the power levers 
below the flight idle stop while the airplane is in flight.

Comments

    Interested persons have been afforded an opportunity to participate 
in the making of this amendment. Due consideration has been given to 
the single comment received.
    The commenter supports the proposed rule.

Conclusion

    After careful review of the available data, including the comment 
noted above, the FAA has determined that air safety and the public 
interest require the adoption of the rule as proposed.

Interim Action

    This is considered interim action until final action is identified, 
at which time the FAA may consider further rulemaking.

Cost Impact

    There are approximately 143 Gulfstream Model G-159 (G-I) airplanes 
of the affected design in the worldwide fleet. The FAA estimates that 
63 airplanes of U.S. registry will be affected by this AD, that it will 
take approximately 1 work hour per airplane to accomplish the required 
actions, and that the average labor rate is $60 per work hour. Based on 
these figures, the cost impact of the AD on U.S. operators is estimated 
to be $3,780, or $60 per airplane.
    The cost impact figure discussed above is based on assumptions that 
no operator has yet accomplished any of the requirements of this AD 
action, and that no operator would accomplish those actions in the 
future if this AD were not adopted.

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 final evaluation has been prepared for this action 
and it is contained in the Rules Docket. A copy of it may be obtained 
from the Rules Docket at the location provided under the caption 
ADDRESSES.

List of Subjects in 14 CFR Part 39

    Air transportation, Aircraft, Aviation safety, 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 U.S.C. 106(g), 40113, 44701.


Sec. 39.13  [Amended]

    2. Section 39.13 is amended by adding the following new 
airworthiness directive:

98-13-30  Gulfstream Aerospace Corporation (Formerly Grumman): 
Amendment 39-10621. Docket 97-NM-302-AD.
    Applicability: All Model G-159 (G-I) airplanes, 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 (b) 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 prevent loss of airplane controllability or engine overspeed 
with consequent loss of engine power, caused by the power levers 
being positioned below the flight idle stop while the airplane is in 
flight, accomplish the following:
    (a) For turbopropeller-powered Gulfstream Model G-159 (G-1) 
airplanes: Within 30 days after the effective date of this AD, 
revise the Limitations Section of the FAA-approved Airplane Flight 
Manual (AFM) to include the following statements. This action may be 
accomplished by inserting a copy of this AD into the AFM.
    ``Positioning of the propeller flight fine pitch lock selector 
to the ground interlock position in flight is PROHIBITED. Such 
positioning may lead to loss of airplane control.''
    (b) 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, FAA, Small Airplane Directorate, 
Atlanta Aircraft Certification Office (ACO). Operators shall submit 
their requests through an appropriate FAA Principal Operations 
Inspector, who may add comments and then send it to the Manager, 
Atlanta ACO.

    Note 2: Information concerning the existence of approved 
alternative methods of compliance with this AD, if any, may be 
obtained from the Atlanta ACO.
    (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) This amendment becomes effective on July 29, 1998.

    Issued in Renton, Washington, on June 16, 1998.
Darrell M. Pederson,
Acting Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 98-16493 Filed 6-23-98; 8:45 am]
BILLING CODE 4910-13-P