[Federal Register Volume 59, Number 51 (Wednesday, March 16, 1994)]
[Unknown Section]
[Page 0]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 94-6042]


[[Page Unknown]]

[Federal Register: March 16, 1994]


-----------------------------------------------------------------------


DEPARTMENT OF TRANSPORTATION
14 CFR Part 39

[Docket No. 91-CE-76-AD]

 

Airworthiness Directives: Beech Aircraft Corp. Models B300 and 
B300C Airplanes

AGENCY: Federal Aviation Administration, DOT.

ACTION: Notice of proposed rulemaking (NPRM).

-----------------------------------------------------------------------

SUMMARY: This document proposes to revise AD 91-20-14, which currently 
requires incorporating revised takeoff and climb performance charts 
into the Pilot's Operating Handbook and FAA Approved Airplane Flight 
Manual (AFM/POH) on Beech Aircraft Corporation (Beech) Models B300 and 
B300C airplanes. Beech has started incorporating these takeoff and 
climb requirements into the AFM/POH of airplanes manufactured since 
issuance of AD 91-20-14. The proposed action would limit the 
applicability to only those airplanes without these takeoff and climb 
requirements incorporated into the AFM/POH at production. The actions 
specified by the proposed AD are intended to ensure that the affected 
airplanes achieve required minimum takeoff and climb performance for 
each approved combination of takeoff configuration, weight, pressure 
altitude, and temperature.

DATES: Comments must be received on or before May 27, 1994.

ADDRESSES: Submit comments in triplicate to the Federal Aviation 
Administration (FAA), Central Region, Office of the Assistant Chief 
Counsel, Attention: Rules Docket No. 91-CE-76-AD, Room 1558, 601 E. 
12th Street, Kansas City, Missouri 64106. Comments may be inspected at 
this location between 8 a.m. and 4 p.m., Monday through Friday, 
holidays excepted.
    Copies of the AFM/POH revision that applies to the proposed AD may 
be obtained from the Beech Aircraft Corporation, P.O. Box 85, Wichita, 
Kansas 67201-0085. This information also may be examined at the Rules 
Docket at the address above.

FOR FURTHER INFORMATION CONTACT: Mr. Bennett L. Sorensen, Flight Test 
Pilot, Wichita Aircraft Certification Office, FAA, 1801 Airport Road, 
Mid-Continent Airport, Wichita, Kansas 67209; telephone (316) 946-4165; 
facsimile (316) 946-4407.

SUPPLEMENTARY INFORMATION:

Comments Invited

    Interested persons are invited to participate in the making of the 
proposed rule by submitting such written data, views, or arguments as 
they may desire. Communications should identify the Rules Docket number 
and be submitted in triplicate to the address specified above. All 
communications received on or before the closing date for comments, 
specified above, will be considered before taking action on the 
proposed rule. The proposals contained in this notice may be changed in 
light of the comments received.
    Comments are specifically invited on the overall regulatory, 
economic, environmental, and energy aspects of the proposed rule. All 
comments submitted will be available, both before and after the closing 
date for comments, in the Rules Docket for examination by interested 
persons. A report that summarizes each FAA-public contact concerned 
with the substance of this proposal will be filed in the Rules Docket.
    Commenters wishing the FAA to acknowledge receipt of their comments 
submitted in response to this notice must submit a self-addressed, 
stamped postcard on which the following statement is made: ``Comments 
to Docket No. 91-CE-76-AD.'' The postcard will be date stamped and 
returned to the commenter.

Availability of NPRMs

    Any person may obtain a copy of this NPRM by submitting a request 
to the FAA, Central Region, Office of the Assistant Chief Counsel, 
Attention: Rules Docket No. 91-CE-76-AD, Room 1558, 601 E. 12th Street, 
Kansas City, Missouri 64106.

Discussion

    AD 91-20-14, Amendment 39-8168 (January 30, 1992, 57 FR 3516), 
currently requires incorporating revised takeoff and climb performance 
charts, B2 revision, part number (P/N) 130-590031-1, dated September 
1991, into the AFM/POH on Beech Models B300 and B300C airplanes. Beech 
has started incorporating these takeoff and climb requirements into the 
AFM/POH of Models B300 and B300C airplanes manufactured since issuance 
of AD 91-20-14.
    After examining the circumstances and reviewing all available 
information related to the action described above, the FAA has 
determined that (1) the applicability of AD 91-20-14 should exclude 
those airplanes incorporating the takeoff and climb requirements in the 
AFM/POH at manufacture; and (2) AD action should remain for all other 
Models B300 and B300C airplanes in order to continue to ensure that 
these airplanes achieve required minimum takeoff and climb performance 
for each approved combination of takeoff configuration, weight, 
pressure altitude, and temperature.
    Since an unsafe condition has been identified that is likely to 
exist or develop in other Beech Models B300 and B300C airplanes of the 
same type design, the proposed AD would revise AD 91-20-14 to continue 
to require incorporating revised takeoff and climb performance charts, 
B2 revision, part number (P/N) 130-590031-1, dated September 1991, into 
the AFM/POH, but would exclude those airplanes incorporating the 
takeoff and climb requirements at manufacture.
    The FAA estimates that 118 airplanes in the U.S. registry would be 
affected by the proposed AD, and that it would take approximately 1 
workhour to incorporate the charts into the POH. Since an owner/
operator who holds a private pilot certificate as authorized by 14 CFR 
43.7 and 14 CFR 43.11 of the Federal Aviation Regulations is allowed to 
accomplish the proposed inspection, the only cost impact upon the 
public would be the time it takes to incorporate these charts.
    The regulations proposed herein would 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 
proposal would 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) if promulgated, 
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 draft regulatory evaluation 
prepared for this action has been placed 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, Safety.

The Proposed Amendment

    Accordingly, pursuant to the authority delegated to me by the 
Administrator, the Federal Aviation Administration proposes to amend 14 
CFR part 39 of the Federal Aviation Regulations as follows:

PART 39--AIRWORTHINESS DIRECTIVES

    1. The authority citation for part 39 continues to read as follows:

    Authority: 49 U.S.C. App. 1354(a), 1421 and 1423; 49 U.S.C. 
106(g); and 14 CFR 11.89.


Sec. 39.13  [Amended]

    2. Section 39.13 is amended by removing AD 91-20-14, Amendment 39-
8168 (January 30, 1992, 57 FR 3516), and by adding the following new 
airworthiness directive to read as follows:

Beech Aircraft Corporation: Docket No. 91-CE-76-AD; Revises AD 91-
20-14, Amendment 39-8168.

    Applicability: The following model and serial number airplanes, 
certificated in any category:

------------------------------------------------------------------------
               Model                              Serial No.            
------------------------------------------------------------------------
B300...............................  FL-1 through FL-110.               
B300C..............................  FM-1 through FM-8.                 
------------------------------------------------------------------------

    Compliance: Required within 10 hours time-in-service after 
February 20, 1992 (the effective date of AD 91-20-14), unless 
already accomplished.
    To ensure that the affected airplanes achieve required minimum 
takeoff and climb performance for each approved combination of 
takeoff configuration, weight, pressure altitude, and temperature, 
accomplish the following:
    (a) Incorporate the takeoff and climb performance charts, B2 
revision, part number (P/N) 130-590031-1, dated September 1991, into 
the Model B300 and B300C Pilot's Operating Handbook and FAA Approved 
Airplane Flight Manual (AFM/POH).

    Note 1: The charts sent in the priority letter AD 91-20-14 
package and B2 revision, P/N 130-590031-1, dated September 1991, are 
the same.

    (b) Incorporating the climb and takeoff charts as required by 
this AD may be performed by the owner/operator holding at least a 
private pilot certificate as authorized by 14 CFR 43.7, and must be 
entered into the aircraft records showing compliance with this AD in 
accordance with 14 CFR 43.11.
    (c) Special flight permits may be issued in accordance with 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 equivalent level of safety may be 
approved by the Manager, Wichita Aircraft Certification Office 
(ACO), FAA, 1801 Airport Road, Room 100, Wichita, Kansas 67209. The 
request should be forwarded through an appropriate FAA Maintenance 
Inspector, who may add comments and send it to the Manager, Wichita 
ACO.

    Note 2: Information concerning the existence of approved 
alternative methods of compliance with this AD, if any, may be 
obtained from the Wichita ACO.

    (e) All persons affected by this directive may obtain copies of 
the AFM/POH revision referred to herein upon request to Beech 
Aircraft Corporation, P.O. Box 85, Wichita, Kansas 67201-0085; or 
may examine these documents at the FAA, Central Region, Office of 
the Assistant Chief Counsel, Room 1558, 601 E. 12th Street, Kansas 
City, Missouri 64106.
    (f) This amendment revises AD 91-20-14, Amendment 39-8168.

    Issued in Kansas City, Missouri, on March 10, 1994.
Barry D. Clements,
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 94-6042 Filed 3-15-94; 8:45 am]
BILLING CODE 4910-13-V